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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Built Environ.</journal-id>
<journal-title>Frontiers in Built Environment</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Built Environ.</abbrev-journal-title>
<issn pub-type="epub">2297-3362</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">790584</article-id>
<article-id pub-id-type="doi">10.3389/fbuil.2021.790584</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Built Environment</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>A Simple Critical Response Evaluation Method for Base-Isolation Building-Connection Hybrid System Under Double Impulse as Representative of Near-Fault Ground Motion</article-title>
<alt-title alt-title-type="left-running-head">Nakamura et&#x20;al.</alt-title>
<alt-title alt-title-type="right-running-head">Base-Isolation Building-Connection Hybrid</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Nakamura</surname>
<given-names>Tomoya</given-names>
</name>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Fujita</surname>
<given-names>Kohei</given-names>
</name>
<uri xlink:href="https://loop.frontiersin.org/people/212313/overview"/>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Takewaki</surname>
<given-names>Izuru</given-names>
</name>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/166204/overview"/>
</contrib>
</contrib-group>
<aff>Department of Architecture and Architectural Engineering, Graduate School of Engineering, Kyoto University, <addr-line>Kyoto</addr-line>, <country>Japan</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/287812/overview">Ehsan Noroozinejad Farsangi</ext-link>, Graduate University of Advanced Technology,&#x20;Iran</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1510074/overview">Alireza Tabrizikahou</ext-link>, Pozna&#x144; University of Technology, Poland</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1513509/overview">Vahidreza Gharehbaghi</ext-link>, University of Southern Queensland, Australia</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Izuru Takewaki, <email>takewaki@archi.kyoto-u.ac.jp</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Earthquake Engineering, a section of the journal Frontiers in Built Environment</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>09</day>
<month>11</month>
<year>2021</year>
</pub-date>
<pub-date pub-type="collection">
<year>2021</year>
</pub-date>
<volume>7</volume>
<elocation-id>790584</elocation-id>
<history>
<date date-type="received">
<day>07</day>
<month>10</month>
<year>2021</year>
</date>
<date date-type="accepted">
<day>22</day>
<month>10</month>
<year>2021</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2021 Nakamura, Fujita and Takewaki.</copyright-statement>
<copyright-year>2021</copyright-year>
<copyright-holder>Nakamura, Fujita and Takewaki</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these&#x20;terms.</p>
</license>
</permissions>
<abstract>
<p>We revisit a unique building system including a base-isolation, building-connection hybrid control system. The base-isolation system withstands pulse-type earthquake ground motions effectively and the building-connection system resists long-duration earthquake ground motions efficiently. A simple smart critical response evaluation method without nonlinear time-history response analysis is proposed for this hybrid building system under near-fault ground motions. An analytical expression of the maximum elastic-plastic deformation of a damped bilinear hysteretic single-degree-of-freedom (SDOF) model under critical double impulse as a representative of pulse-type ground motions derived in our previous paper plays an important role in the development of the simple critical response evaluation method. A two-step transformation procedure into an SDOF model is proposed. The first step is the transformation of the main base-isolated building into an SDOF system and the second step is the reduction of the connecting dampers supported on a sub building to a damper with a sophisticated compensation factor on an assumed rigid wall. The evaluation of damping coefficients with the consideration of yielding of the base-isolation story is a key step in this paper. Different from the previous work, the equivalent damping coefficient is derived depending on the response range before and after yielding of the base-isolation story. This treatment enhances the accuracy of the proposed method. The accuracy and reliability of the proposed response evaluation method is demonstrated by the time-history response analysis of the multi-degree-of-freedom (MDOF)&#x20;model.</p>
</abstract>
<kwd-group>
<kwd>base-isolation</kwd>
<kwd>building-connection</kwd>
<kwd>hybrid control</kwd>
<kwd>passive control</kwd>
<kwd>near-fault ground motion</kwd>
<kwd>double impulse</kwd>
<kwd>critical response</kwd>
</kwd-group>
<contract-sponsor id="cn001">Japan Society for the Promotion of Science<named-content content-type="fundref-id">10.13039/501100001691</named-content>
</contract-sponsor>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>The resilience of building structures during and after natural disasters is a central theme of late, and many investigations have been accumulated (<xref ref-type="bibr" rid="B7">Bruneau and Reinhorn, 2006</xref>; <xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>). <xref ref-type="bibr" rid="B7">Bruneau and Reinhorn (2006)</xref> introduced four factors (redundancy, robustness, rapidity, and resourcefulness) to characterize structure resilience. In earthquake-prone countries and regions, it is essential to design building structures so as to resist severe earthquakes without major damage that obstructs their continuing use (<xref ref-type="bibr" rid="B3">Amadio et&#x20;al., 2003</xref>; <xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>; <xref ref-type="bibr" rid="B38">Takewaki, 2013</xref>; <xref ref-type="bibr" rid="B41">Takewaki et&#x20;al., 2013</xref>). Since intrinsically uncertain characteristics of earthquake ground motions are inevitable, the reliable prediction of forthcoming events in regards to time, space, and character is extremely difficult (<xref ref-type="bibr" rid="B38">Takewaki, 2013</xref>; <xref ref-type="bibr" rid="B42">Takewaki et&#x20;al., 2011</xref>; <xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>; <xref ref-type="bibr" rid="B41">Takewaki et&#x20;al., 2013</xref>). Although newer buildings systems such as passive control systems and base-isolation systems are anticipated as effective strategies for guaranteeing the structural safety of building structures, the structural properties of constituent members and elements of such innovative systems are not certain (<xref ref-type="bibr" rid="B6">Ben-Haim, 2006</xref>; <xref ref-type="bibr" rid="B8">Fujita et&#x20;al., 2021</xref>). In Japan, the consideration of the variabilities of structural properties of isolators and dampers is mandatory in the design of passively controlled buildings and base-isolated buildings because the uncertainty degree (<inline-formula id="inf1">
<mml:math id="m1">
<mml:mo>&#xb1;</mml:mo>
</mml:math>
</inline-formula> 20&#x2013;30%) of isolators and dampers is usually larger than those of building frame members (beams and columns) (<xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>; <xref ref-type="bibr" rid="B8">Fujita et&#x20;al., 2021</xref>). The concept of robustness and redundancy plays a central role in the resilient seismic-resistant design of such building structures (<xref ref-type="bibr" rid="B6">Ben-Haim, 2006</xref>; <xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>; <xref ref-type="bibr" rid="B8">Fujita et&#x20;al., 2021</xref>). In the field of resilience, the theme of &#x201c;Community Resilience&#x201d; is receiving much interest recently because of the complexity of the concept of resilience and the difficulty in its realization in a real community consisting of many built environments (<xref ref-type="bibr" rid="B31">Mieler et&#x20;al., 2015</xref>; <xref ref-type="bibr" rid="B28">Masoomi and van de Lindt, 2019</xref>; <xref ref-type="bibr" rid="B46">You et&#x20;al., 2021</xref>).</p>
<p>Since the 1980s, base-isolated buildings have been developed rapidly. They are effective for pulse-type ground motions with predominant periods shorter than a few seconds or random earthquake ground motions (<xref ref-type="bibr" rid="B11">Hall et&#x20;al., 1995</xref>; <xref ref-type="bibr" rid="B16">Jangid, 1995</xref>; <xref ref-type="bibr" rid="B21">Kelly, 1999</xref>; <xref ref-type="bibr" rid="B33">Naeim and Kelly, 1999</xref>; <xref ref-type="bibr" rid="B15">Jangid and Kelly, 2001</xref>; <xref ref-type="bibr" rid="B14">Hino et&#x20;al., 2008</xref>; <xref ref-type="bibr" rid="B40">Takewaki and Fujita, 2009</xref>). However, their earthquake resilience is not completely guaranteed for long-period ground motions with a predominant period of 5&#x2013;8&#xa0;s (<xref ref-type="bibr" rid="B18">Kamae et&#x20;al., 2004</xref>; <xref ref-type="bibr" rid="B4">Ariga et&#x20;al., 2006</xref>). Although it is believed in general that passive energy dissipating systems (especially connected building systems) are effective for long-duration and long-period ground motions due to allowing sufficient time for energy dissipation (<xref ref-type="bibr" rid="B26">Luco and Barros, 1998</xref>; <xref ref-type="bibr" rid="B5">Basili and Angelis, 2007</xref>; <xref ref-type="bibr" rid="B39">Takewaki, 2007</xref>; <xref ref-type="bibr" rid="B34">Patel and Jangid, 2011</xref>; <xref ref-type="bibr" rid="B42">Takewaki et&#x20;al., 2011</xref>; <xref ref-type="bibr" rid="B37">Takewaki et&#x20;al., 2012</xref>; <xref ref-type="bibr" rid="B35">Richardson et&#x20;al., 2013</xref>; <xref ref-type="bibr" rid="B9">Fukumoto and Takewaki, 2015</xref>; <xref ref-type="bibr" rid="B20">Kawai et&#x20;al., 2021</xref>), they are not necessarily resilient against impulsive pulse-type ground motions.</p>
<p>In this paper, a new kind of hybrid or dual passive control building systems is treated in which a base-isolated building model is supported by a sub building (e.g., car parking tower) through oil dampers (<xref ref-type="bibr" rid="B32">Murase et&#x20;al., 2013</xref>; <xref ref-type="bibr" rid="B19">Kasagi et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B10">Fukumoto and Takewaki 2017</xref>). Some researchers demonstrated that this new passive control system is effectively robust for two counterpart-type earthquake ground motions, i.e.,&#x20;pulse-type ground motions and long-duration, long-period ground motions (<xref ref-type="bibr" rid="B32">Murase et&#x20;al., 2013</xref>; <xref ref-type="bibr" rid="B19">Kasagi et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B10">Fukumoto and Takewaki 2017</xref>). It has also been demonstrated through the input energy analysis in the frequency domain that, although the connecting oil dampers do not withstand pulse-type ground motions effectively due to the lack of time for energy dissipation, those dampers work smartly for long-duration, long-period ground motions (<xref ref-type="bibr" rid="B44">Taniguchi et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B43">Tamura et&#x20;al., 2017</xref>). However, these analyses are limited to linear models. Although <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> and <xref ref-type="bibr" rid="B12">Hayashi et&#x20;al. (2018)</xref> developed a simple method using a single-degree-of-freedom (SDOF) model for simulating the earthquake response of these buildings including the base-isolation, building connection hybrid damper system of nonlinear properties, the accuracy for near-fault ground motions is relatively low because of the non-robust evaluation of damping properties (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>), or the method was applied only to the response under long-duration ground motion (<xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>).</p>
<p>A simple and sophisticated response evaluation method using an SDOF model is proposed in this paper for the above-mentioned base-isolation, building-connection hybrid structural system under a near-fault ground motion. As in the previous method (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>; <xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>), a two-step transformation of the overall structural system into an SDOF model is conducted. The first step is the transformation into an SDOF system and the second step is the reduction of the connecting oil dampers supported on a sub building to upper-story concentrated oil dampers with a smart compensation factor on a rigid wall. It is shown that application of the previously derived analytical expression (<xref ref-type="bibr" rid="B1">Akehashi et&#x20;al., 2018</xref>) of the maximum deformation to the reduced SDOF model under the critical double impulse as a representative of pulse-type near-fault ground motions enables the establishment of a simplified, but rather accurate response evaluation method.</p>
</sec>
<sec id="s2">
<title>2 Double Impulse as Representative of Near-Fault Ground Motion</title>
<sec id="s2-1">
<title>2.1 Transformation of the Main Part of Near-Fault Ground Motion into Double Impulse</title>
<p>The concept of a pair of impulses with inverse directions to each other, called a double impulse, was introduced by <xref ref-type="bibr" rid="B23">Kojima and Takewaki (2015a)</xref> to represent a major part of near-fault ground motions. Since the characteristic main part of near-fault ground motions is well known to be expressed by a pulse-type one-cycle or 1.5-cycle sine wave and is influential particularly for tall and base-isolated buildings, with a rather long natural period (<xref ref-type="bibr" rid="B36">Sasani and Bertero, 2000</xref>; <xref ref-type="bibr" rid="B30">Mavroeidis and Papageorgiou, 2003</xref>; <xref ref-type="bibr" rid="B27">Makris and Black, 2004</xref>; <xref ref-type="bibr" rid="B29">Mavroeidis et&#x20;al., 2004</xref>; <xref ref-type="bibr" rid="B17">Kalkan and Kunnath, 2006</xref>). <xref ref-type="fig" rid="F1">Figure&#x20;1A</xref> shows an example of a near-fault ground motion (Rinaldi FN component during the 1994 Northridge earthquake) and its modeling into a one-cycle sine wave and a double impulse. <xref ref-type="fig" rid="F1">Figure&#x20;1B</xref> illustrates the velocity and displacement properties of the one-cycle sine wave and the double impulse. The red arrows indicate the Dirac delta function <inline-formula id="inf2">
<mml:math id="m2">
<mml:mrow>
<mml:mi>&#x3b4;</mml:mi>
<mml:mrow>
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</inline-formula>. <italic>V</italic> is the given velocity (the input velocity level) and <inline-formula id="inf3">
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</inline-formula> is the time interval of two impulses. Consequently, the double impulse can be expressed by<disp-formula id="e1">
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</mml:mrow>
</mml:math>
<label>(1)</label>
</disp-formula>
</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Transformation of recorded ground motion into a one-cycle sine wave and double impulse, <bold>(A)</bold> Example of Rinaldi Station FN component during 1994 Northridge earthquake and its modeling into a one-cycle sine wave and double impulse, <bold>(B)</bold> Velocity and displacement properties of a one-cycle sine wave and double impulse.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g001.tif"/>
</fig>
<p>To make the double impulse a reliable substitute for near-fault ground motions, it is important to compare it with the one-cycle sine wave. The equivalent one-cycle sine wave with the circular frequency <inline-formula id="inf4">
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</mml:mrow>
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</inline-formula> (the period is <inline-formula id="inf5">
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</inline-formula>) and the velocity amplitude <inline-formula id="inf6">
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<mml:mn>1</mml:mn>
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</inline-formula> can be expressed by<disp-formula id="e2">
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</mml:msub>
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</mml:mrow>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(2)</label>
</disp-formula>where <inline-formula id="inf7">
<mml:math id="m9">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">V</mml:mi>
<mml:mrow>
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</inline-formula> (<xref ref-type="bibr" rid="B22">Kojima et&#x20;al., 2018</xref>). This relation can be derived from the equivalence of the maximum Fourier amplitudes of both inputs.</p>
</sec>
</sec>
<sec id="s3">
<title>3 Summary of Previous Research for Accuracy Upgrade</title>
<p>The base-isolation, building-connection hybrid control system as shown in <xref ref-type="fig" rid="F2">Figure&#x20;2A</xref> was treated by <xref ref-type="bibr" rid="B32">Murase et&#x20;al. (2013)</xref>. They demonstrated the high performance of this control system for both impulsive and long-duration ground motions. Then, <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> tried to propose a simple response evaluation method using an SDOF model for impulsive and long-duration ground motions (<xref ref-type="bibr" rid="B24">Kojima and Takewaki, 2015b</xref>). It was shown that, while his simple model is effective for long-duration ground motions (<xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>), it is not for impulsive ground motions resulting from the narrow-band estimation performance of the equivalent damping for a broader range of deformation including a plastic region. In this paper, a revised transformation method effective also for impulsive ground motions is presented. For this purpose, the method by <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> is explained&#x20;first.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Base-isolation, building-connection hybrid control system, <bold>(A)</bold> Overview of system (<xref ref-type="bibr" rid="B10">Fukumoto and Takewaki, 2017</xref>), <bold>(B)</bold> MDOF shear building model with the base-isolation, building-connection hybrid control system, <bold>(C)</bold> Restoring force-deformation relation of the base-isolation&#x20;story.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g002.tif"/>
</fig>
<p>Consider a multi-degree-of-freedom (MDOF) shear building model with the base-isolation, building-connection hybrid control system as shown in <xref ref-type="fig" rid="F2">Figure&#x20;2B</xref>. The common mass of the main building, the common mass of the sub building, and the mass of the base-isolation story are denoted by <inline-formula id="inf8">
<mml:math id="m10">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf9">
<mml:math id="m11">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>F</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf10">
<mml:math id="m12">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. The damping coefficient of each connecting viscous damper is <inline-formula id="inf11">
<mml:math id="m13">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula>. The base-isolation story is assumed to consist of natural rubber isolators, steel dampers, and oil dampers. By neglecting the second-branch stiffness (stiffness of natural rubber after yielding of steel dampers), the restoring-force characteristic of the base-isolation story is assumed to obey an elastic-perfectly plastic model as shown in <xref ref-type="fig" rid="F2">Figure&#x20;2C</xref>. The story shear force and the deformation of the base-isolation story are denoted by <inline-formula id="inf12">
<mml:math id="m14">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">Q</mml:mi>
<mml:mi mathvariant="italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf13">
<mml:math id="m15">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. The initial stiffness, the yield force, and the yield deformation of the base-isolation story are expressed by <inline-formula id="inf14">
<mml:math id="m16">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">f</mml:mi>
<mml:mi mathvariant="italic">y</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">d</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">yI</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the damping coefficient of the base-isolation story is denoted by&#x20;<inline-formula id="inf15">
<mml:math id="m17">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
<p>In the method of <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref>, an elastic-perfectly plastic SDOF model with viscous damping was introduced to make use of an effective response evaluation method by the critical (resonant) double impulse (<xref ref-type="bibr" rid="B22">Kojima et&#x20;al., 2018</xref>).</p>
<p>In the single base-isolated building, the superstructure is modeled into an SDOF model and a 2DOF model is constructed with the super building model mass <inline-formula id="inf16">
<mml:math id="m18">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the base-isolation story mass <inline-formula id="inf17">
<mml:math id="m19">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">m</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. By neglecting <inline-formula id="inf18">
<mml:math id="m20">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> compared to <inline-formula id="inf19">
<mml:math id="m21">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> in high-rise buildings, the base-isolated building is reduced to an SDOF model. The super building model mass <inline-formula id="inf20">
<mml:math id="m22">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the sum of the super building masses. The stiffness <inline-formula id="inf21">
<mml:math id="m23">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the damping coefficient <inline-formula id="inf22">
<mml:math id="m24">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the super building are determined so as to attain the given fundamental natural period and the specified lowest damping ratio of the MDOF model. <inline-formula id="inf23">
<mml:math id="m25">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">f</mml:mi>
<mml:mi mathvariant="italic">y</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">d</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">yI</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, and <inline-formula id="inf24">
<mml:math id="m26">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> defined above for the MDOF model are used in the 2DOF model <inline-formula id="inf25">
<mml:math id="m27">
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">f</mml:mi>
<mml:mi mathvariant="italic">y</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">d</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">yI</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mrow>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>. In the SDOF model, the mass, the initial stiffness, the yield deformation, and the damping coefficient are expressed by <inline-formula id="inf26">
<mml:math id="m28">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf27">
<mml:math id="m29">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf28">
<mml:math id="m30">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">d</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">ye</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf29">
<mml:math id="m31">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
<p>By applying the above-mentioned assumption, the mass of the SDOF model is obtained as<disp-formula id="e3">
<mml:math id="m32">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>The series-spring assumption leads to the following initial stiffness of the SDOF model.<disp-formula id="e4">
<mml:math id="m33">
<mml:mrow>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<p>As for the damping, the series-spring assumption of complex springs provides the damping coefficient <inline-formula id="inf30">
<mml:math id="m34">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model (<xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>).<disp-formula id="e5">
<mml:math id="m35">
<mml:mrow>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>where i is the imaginary unit and<disp-formula id="e6">
<mml:math id="m36">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
<mml:mo>/</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:msqrt>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<p>From <xref ref-type="disp-formula" rid="e5">Eqs 5</xref>, <xref ref-type="disp-formula" rid="e6">6</xref>, <inline-formula id="inf31">
<mml:math id="m37">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> can be derived consequently as<disp-formula id="e7">
<mml:math id="m38">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msubsup>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
<mml:mn>2</mml:mn>
</mml:msubsup>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
<mml:mrow>
<mml:msup>
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>&#x3c9;</mml:mi>
<mml:mi mathvariant="italic">e</mml:mi>
<mml:mn>2</mml:mn>
</mml:msubsup>
<mml:msup>
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">I</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfrac>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(7)</label>
</disp-formula>
</p>
<p>The problem in deriving <inline-formula id="inf32">
<mml:math id="m39">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">c</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">main</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is that the effect of yielding in the base-isolation story is not reflected. This issue will be overcome in this paper. On the other hand, the reduction of connecting dampers requires a sophisticated procedure which considers 1) the effect of rigid modeling of the sub building for simple treatment, 2) the effect of the location of connecting dampers, 3) the effect of height of the sub building. <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> introduced a coefficient <inline-formula id="inf33">
<mml:math id="m40">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi mathvariant="italic">d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> on the connecting damping coefficient <inline-formula id="inf34">
<mml:math id="m41">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> for compensating these effects in the model where the connecting dampers are allocated in the top <inline-formula id="inf35">
<mml:math id="m42">
<mml:mrow>
<mml:msub>
<mml:mi>n</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> stories and the main building is connected to the sub building at the top <inline-formula id="inf36">
<mml:math id="m43">
<mml:mrow>
<mml:msub>
<mml:mi>n</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> stories (this model is called the RMDOF model). Consequently, the total connecting damping coefficient is determined by<disp-formula id="e8">
<mml:math id="m44">
<mml:mrow>
<mml:mi>C</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>n</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mi>c</mml:mi>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(8)</label>
</disp-formula>
</p>
<p>The compensation coefficient <inline-formula id="inf37">
<mml:math id="m45">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is determined so that the fundamental damping ratios of the MDOF model and the RMDOF model by complex eigenvalue analysis coincide. In the analysis, the equivalent stiffness <inline-formula id="inf38">
<mml:math id="m46">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story is to be evaluated iteratively for the convergent deformation <inline-formula id="inf39">
<mml:math id="m47">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation&#x20;story.</p>
</sec>
<sec id="s4">
<title>4 A Simple Critical Response Evaluation Method for Base-Isolated Building Under Double Impulse as Representative of Near-Fault Ground Motion</title>
<p>As explained before, it was shown that, while Hayashi&#x2019;s simple model (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>) is effective for long-duration ground motions (<xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>), it is not for impulsive ground motions. In this paper, a revised transformation method effective for even impulsive ground motions is presented.</p>
<sec id="s4-1">
<title>4.1 Plane Frame Model of Base-Isolated High-Rise Building</title>
<p>Consider a 40-story base-isolated frame building model as shown in <xref ref-type="fig" rid="F3">Figure&#x20;3</xref>. Unlike the base-isolation system used in <xref ref-type="sec" rid="s3">Section 3</xref>, lead rubber isolators and oil dampers are employed as the constituent members of the base-isolated story. The total depth of these isolators is 200 [mm]. This base-isolated frame building model is reduced to an SDOF mass-spring model with a dashpot via a 2DOF model as illustrated in <xref ref-type="fig" rid="F3">Figure&#x20;3</xref>. For the simplicity of presentation of the proposed theory, the super building frame has a constant floor mass <inline-formula id="inf40">
<mml:math id="m48">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the free wall (sub building) has a constant floor mass <inline-formula id="inf41">
<mml:math id="m49">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>F</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. Let <inline-formula id="inf42">
<mml:math id="m50">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> denote the mass of the base-isolation story and let <inline-formula id="inf43">
<mml:math id="m51">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> denote the constant damping coefficient of connecting oil dampers placed at several stories. The base-isolation story is assumed to have a bilinear hysteretic restoring-force characteristic as usually used for lead rubber isolators. <inline-formula id="inf44">
<mml:math id="m52">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> indicate the initial stiffness in the elastic range, the yield force, and the yield deformation of the base-isolation story, respectively <inline-formula id="inf45">
<mml:math id="m53">
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mrow>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>. The first and second stiffnesses of each lead rubber isolator are <inline-formula id="inf46">
<mml:math id="m54">
<mml:mrow>
<mml:msub>
<mml:mi>K</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>20.01</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> [kN/mm] and <inline-formula id="inf47">
<mml:math id="m55">
<mml:mrow>
<mml:msub>
<mml:mi>K</mml:mi>
<mml:mn>2</mml:mn>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.54</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> [kN/mm] and the force axis percept is <inline-formula id="inf48">
<mml:math id="m56">
<mml:mrow>
<mml:msub>
<mml:mi>Q</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
</mml:mrow>
</mml:math>
</inline-formula> <inline-formula id="inf49">
<mml:math id="m57">
<mml:mrow>
<mml:mn>360.6</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> [kN]. These properties are multiplied by 36 (number of lead rubber bearings) to obtain the restoring-force characteristics of the base-isolation&#x20;story.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Reduction of base-isolated tall plane frame into SDOF&#x20;model.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g003.tif"/>
</fig>
<p>
<inline-formula id="inf50">
<mml:math id="m58">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mi>u</mml:mi>
<mml:mi>p</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf51">
<mml:math id="m59">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>b</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> denote the fundamental natural period of the main frame building for the fixed base-isolation story and the fundamental natural period of the sub building. Furthermore, <inline-formula id="inf52">
<mml:math id="m60">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> indicates the total damping coefficient of oil dampers in the base-isolation story. The total damping coefficient <inline-formula id="inf53">
<mml:math id="m61">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of oil dampers is to be specified so as to attain the damping ratio 0.15 for the equivalent stiffness <inline-formula id="inf54">
<mml:math id="m62">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story at the deformation <inline-formula id="inf55">
<mml:math id="m63">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.4</mml:mn>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mtext>m</mml:mtext>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>. The structural damping ratio of the super-structure (instantaneous stiffness-proportional damping) is set to 0.03. The strength of concrete is Fc60 (60&#xa0;[N/mm<sup>2</sup>]) and the Young&#x2019;s modulus is 33,500&#xa0;[N/mm<sup>2</sup>]. The floor mass is 286.2 &#xd7; 10<sup>3</sup>&#xa0;[kg] and the mass of the base-isolation story is 858.6 &#xd7; 10<sup>3</sup>&#xa0;[kg]. The parameters of the base-isolated building are shown in <xref ref-type="table" rid="T1">Table&#x20;1</xref>.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Member parameters of plane&#x20;frame.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" colspan="2" align="left"/>
<th colspan="3" align="center">Column</th>
</tr>
<tr>
<th align="center">B &#xd7; D</th>
<th align="center">Main steel bar</th>
<th align="center">Stirup</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td rowspan="2" align="left">35&#x223c;39 story</td>
<td align="left">outer</td>
<td align="center">850 &#xd7; 950</td>
<td align="center">14-D32</td>
<td align="center">D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">850 &#xd7; 900</td>
<td align="center">14-D29</td>
<td align="center">D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">30&#x223c;34 story</td>
<td align="left">outer</td>
<td align="center">900 &#xd7; 950</td>
<td align="center">14-D32</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">900 &#xd7; 950</td>
<td align="center">14-D29</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">23&#x223c;29 story</td>
<td align="left">outer</td>
<td align="center">900 &#xd7; 950</td>
<td align="center">14-D35</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">950 &#xd7; 950</td>
<td align="center">14-D32</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">18&#x223c;22 story</td>
<td align="left">outer</td>
<td align="center">950 &#xd7; 950</td>
<td align="center">14-D35</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">1,000 &#xd7; 1,000</td>
<td align="center">14-D32</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">13&#x223c;17 story</td>
<td align="left">outer</td>
<td align="center">1,000 &#xd7; 1,050</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">1,000 &#xd7; 1,050</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">7&#x223c;12 story</td>
<td align="left">outer</td>
<td align="center">1,050 &#xd7; 1,100</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">1,000 &#xd7; 1,100</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td rowspan="2" align="left">1&#x223c;6 story</td>
<td align="left">outer</td>
<td align="center">1,100 &#xd7; 1,200</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td align="left">inner</td>
<td align="center">1,050 &#xd7; 1,150</td>
<td align="center">22-D38</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td colspan="2" align="left"/>
<td colspan="3" align="center">
<bold>Beam</bold>
</td>
</tr>
<tr>
<td colspan="2" align="left">30&#x223c;39 story</td>
<td align="center">545 &#xd7; 850</td>
<td align="center">Upper and lower 4-D32</td>
<td align="center">4-D13@200</td>
</tr>
<tr>
<td colspan="2" align="left">23&#x223c;29 story</td>
<td align="center">600 &#xd7; 850</td>
<td align="center">Upper and lower 6-D41</td>
<td align="center">4-D13@100</td>
</tr>
<tr>
<td colspan="2" align="left">1&#x223c;22 story</td>
<td align="center">660 &#xd7; 850</td>
<td align="center">Upper and lower 6-D41</td>
<td align="center">4-D13@100</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s4-2">
<title>4.2 Transformation of Base-Isolated Building Frame into SDOF Model</title>
<p>Consider the transformation of a base-isolated building frame into a 2DOF&#x20;model.</p>
<p>Since the fundamental natural period of the super building with a fixed base is 3.0&#xa0;(s), the stiffness of the super building can be obtained as<disp-formula id="e9">
<mml:math id="m64">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">k</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi mathvariant="italic">M</mml:mi>
<mml:mi mathvariant="italic">U</mml:mi>
</mml:msub>
<mml:msup>
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
<mml:mi>&#x3c0;</mml:mi>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:mn>3.0</mml:mn>
</mml:mrow>
</mml:mrow>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(9)</label>
</disp-formula>
</p>
<p>The initial stiffness <inline-formula id="inf56">
<mml:math id="m65">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the second stiffness <inline-formula id="inf57">
<mml:math id="m66">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story are determined by considering the hysteretic characteristics and the number of isolators and dampers (<xref ref-type="fig" rid="F4">Figure&#x20;4A</xref>). Let <inline-formula id="inf58">
<mml:math id="m67">
<mml:mrow>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf59">
<mml:math id="m68">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> denote the yield deformation and the yield force of the base-isolation story. The damping coefficient of the super building as an SDOF model is determined for the fundamental damping ratio &#x3d; 0.03 by<disp-formula id="e10">
<mml:math id="m69">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>2</mml:mn>
<mml:mo>&#xd7;</mml:mo>
<mml:mn>0.03</mml:mn>
<mml:mo>&#xd7;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:msqrt>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(10)</label>
</disp-formula>
</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Transformation from 2DOF model into SDOF model, <bold>(A)</bold> Force-deformation relation of a base-isolation story in 2DOF model and that in SDOF model, <bold>(B)</bold> Evaluation of deformation of the base-isolation story in SDOF&#x20;model.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g004.tif"/>
</fig>
<p>The damping coefficient of the base-isolation story is determined by considering the number of oil dampers.</p>
<p>The 2DOF model set above is modeled into an SDOF model as shown in <xref ref-type="fig" rid="F3">Figure&#x20;3</xref>. Since <inline-formula id="inf60">
<mml:math id="m70">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is rather small compared to <inline-formula id="inf61">
<mml:math id="m71">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> in high-rise buildings, <inline-formula id="inf62">
<mml:math id="m72">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is neglected here. Then<disp-formula id="e11">
<mml:math id="m73">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(11)</label>
</disp-formula>
</p>
<p>The stiffness and damping coefficient of the SDOF model are determined differently in the elastic region and the plastic region of the base-isolation story. While <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> determined the equivalent damping coefficient only for the initial stiffness, that is determined differently in the elastic region and the plastic region of the base-isolation&#x20;story.</p>
<p>In the region before the yielding of the base-isolation story, the equivalent stiffness <inline-formula id="inf63">
<mml:math id="m74">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the equivalent damping coefficient <inline-formula id="inf64">
<mml:math id="m75">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model can be evaluated by the following series modeling of complex springs.<disp-formula id="e12">
<mml:math id="m76">
<mml:mrow>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(12)</label>
</disp-formula>where <inline-formula id="inf65">
<mml:math id="m77">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the elastic fundamental natural circular frequency of the 2DOF model and the natural circular frequency of the SDOF model is obtained from <inline-formula id="inf66">
<mml:math id="m78">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:msqrt>
</mml:mrow>
</mml:math>
</inline-formula>. From <xref ref-type="disp-formula" rid="e12">Eq. 12</xref>, <inline-formula id="inf67">
<mml:math id="m79">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf68">
<mml:math id="m80">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> are obtained. While <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> obtained the elastic stiffness and the damping coefficient from <xref ref-type="disp-formula" rid="e4">Eqs 4</xref>, <xref ref-type="disp-formula" rid="e5">5</xref>, the proposed method provides those in a unified manner from <xref ref-type="disp-formula" rid="e12">Eq.&#x20;12</xref>.</p>
<p>After the yielding of the steel damper in the base-isolation story, the stiffness reduces to <inline-formula id="inf69">
<mml:math id="m81">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (see <xref ref-type="fig" rid="F4">Figure&#x20;4A</xref>) and the equivalent stiffness in the base-isolation story changes gradually in time. By responding to this phenomenon, assume the deformation <inline-formula id="inf70">
<mml:math id="m82">
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story and the equivalent stiffness of the base-isolation story by<disp-formula id="e13">
<mml:math id="m83">
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(13)</label>
</disp-formula>
<disp-formula id="e14">
<mml:math id="m84">
<mml:mrow>
<mml:msubsup>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
</mml:mrow>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(14)</label>
</disp-formula>where <italic>n</italic> indicates the iteration cycle number. Based on these values, the equivalent stiffness and the equivalent damping coefficient of the SDOF model are obtained from<disp-formula id="e15">
<mml:math id="m85">
<mml:mrow>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mtext>i</mml:mtext>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(15)</label>
</disp-formula>where <inline-formula id="inf71">
<mml:math id="m86">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> denotes the equivalent stiffness of the SDOF model and is defined by<disp-formula id="e16">
<mml:math id="m87">
<mml:mrow>
<mml:msubsup>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msubsup>
</mml:mrow>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(16)</label>
</disp-formula>
<inline-formula id="inf72">
<mml:math id="m88">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is an assumed maximum deformation of the SDOF model and is determined by <inline-formula id="inf73">
<mml:math id="m89">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. In this computation, the lowest mode of the 2DOF model is used so that the equivalent stiffness of the base-isolation story in the 2DOF model attains <inline-formula id="inf74">
<mml:math id="m90">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and defines the deformation of the super building as <inline-formula id="inf75">
<mml:math id="m91">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the deformation <inline-formula id="inf76">
<mml:math id="m92">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation&#x20;story.</p>
<p>In <xref ref-type="disp-formula" rid="e15">Eq. 15</xref>, <inline-formula id="inf77">
<mml:math id="m93">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the fundamental natural circular frequency of the 2DOF model with the equivalent stiffness <inline-formula id="inf78">
<mml:math id="m94">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story. In addition, <inline-formula id="inf79">
<mml:math id="m95">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:msqrt>
</mml:mrow>
</mml:math>
</inline-formula>. From <xref ref-type="disp-formula" rid="e15">Eq. 15</xref>, <inline-formula id="inf80">
<mml:math id="m96">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf81">
<mml:math id="m97">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> are consequently obtained.</p>
<p>Once <inline-formula id="inf82">
<mml:math id="m98">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf83">
<mml:math id="m99">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> are obtained for the SDOF model, the second stiffness <inline-formula id="inf84">
<mml:math id="m100">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model is determined by using the force-deformation relation of the 2DOF model. Since the equivalent damping coefficient of the SDOF model changes depending on the yielding of the base isolation story, <inline-formula id="inf85">
<mml:math id="m101">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the post-yield case is used as the equivalent damping coefficient <inline-formula id="inf86">
<mml:math id="m102">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> in place of <inline-formula id="inf87">
<mml:math id="m103">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the elastic&#x20;case.</p>
<p>Through the above-mentioned procedure, the parameters <inline-formula id="inf88">
<mml:math id="m104">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf89">
<mml:math id="m105">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf90">
<mml:math id="m106">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf91">
<mml:math id="m107">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the SDOF model are obtained.</p>
<p>The maximum deformation of the bilinear hysteretic SDOF model to the critical double impulse was derived by <xref ref-type="bibr" rid="B1">Akehashi et&#x20;al. (2018)</xref>. In this paper, this closed-form expression is used. The relation between <inline-formula id="inf92">
<mml:math id="m108">
<mml:mrow>
<mml:msub>
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<mml:mrow>
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</mml:math>
</inline-formula> is derived as follows.<disp-formula id="e17">
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<mml:mo>&#x3d;</mml:mo>
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<mml:mtable>
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</mml:mtd>
</mml:mtr>
</mml:mtable>
</mml:mrow>
</mml:mrow>
<mml:mo>,</mml:mo>
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</mml:math>
<label>(17)</label>
</disp-formula>
<disp-formula id="e18">
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<mml:msub>
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</mml:mtable>
<mml:mtable>
<mml:mtr>
<mml:mtd>
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</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:mtd>
</mml:mtr>
<mml:mtr>
<mml:mtd>
<mml:mrow>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>max</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2265;</mml:mo>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:mtd>
</mml:mtr>
</mml:mtable>
</mml:mrow>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(18)</label>
</disp-formula>where <inline-formula id="inf94">
<mml:math id="m112">
<mml:mrow>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the yield displacement of the SDOF model and <inline-formula id="inf95">
<mml:math id="m113">
<mml:mrow>
<mml:msub>
<mml:mi>b</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf96">
<mml:math id="m114">
<mml:mrow>
<mml:msub>
<mml:mi>b</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> are the force-axis intercept in the 2DOF model and the SDOF model. Because the SDOF model is modeled from the 2DOF model, the maximum deformation <inline-formula id="inf97">
<mml:math id="m115">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>o</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story has to be transformed from the maximum deformation <inline-formula id="inf98">
<mml:math id="m116">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>max</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model. In this process, the maximum story shear force of the SDOF model is defined by <inline-formula id="inf99">
<mml:math id="m117">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>max</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> , and the deformation <inline-formula id="inf100">
<mml:math id="m118">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>o</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story of the 2DOF model is computed for the same maximum story shear force <inline-formula id="inf101">
<mml:math id="m119">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>max</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (see <xref ref-type="fig" rid="F4">Figure&#x20;4B</xref>).</p>
<p>In <xref ref-type="disp-formula" rid="e14">Eq. 14</xref>, the parameters of the SDOF model are determined for an assumed equivalent stiffness <inline-formula id="inf102">
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<mml:mi>k</mml:mi>
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<mml:mi>e</mml:mi>
<mml:mi>q</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story of the 2DOF model. The assumed maximum deformation <inline-formula id="inf103">
<mml:math id="m121">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the base-isolation story is determined iteratively so that the difference from the value <inline-formula id="inf104">
<mml:math id="m122">
<mml:mrow>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>o</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> obtained from <xref ref-type="disp-formula" rid="e17">Eqs 17</xref>, <xref ref-type="disp-formula" rid="e18">18</xref> is minimized. The flowchart is shown in <xref ref-type="fig" rid="F5">Figure&#x20;5</xref>.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Flow for determining equivalent stiffness.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g005.tif"/>
</fig>
</sec>
<sec id="s4-3">
<title>4.3 Accuracy Check of Proposed Simple Response Evaluation Method Using SDOF Model Through Comparison With Time-History Response Analysis Result for Plane Frame Model</title>
<p>The parameters of the 2DOF model and the SDOF model obtained by the above-mentioned procedure are shown in <xref ref-type="table" rid="T2">Table&#x20;2</xref>.</p>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Parameters of 2DOF model and SDOF model of base-isolated building.</p>
</caption>
<table>
<tbody valign="top">
<tr>
<td rowspan="8" align="left">2DOF</td>
<td rowspan="3" align="left">Super building</td>
<td align="center">
<inline-formula id="inf105">
<mml:math id="m123">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">6.7 &#xd7; 10<sup>7</sup>&#xa0;[kg]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf106">
<mml:math id="m124">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">2.9 &#xd7; 10<sup>8</sup>&#xa0;[N/m]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf107">
<mml:math id="m125">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>U</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">8.4 &#xd7; 10<sup>6</sup>&#xa0;[N/(m/s)]</td>
</tr>
<tr>
<td rowspan="5" align="left">Base-isolation story</td>
<td align="center">
<inline-formula id="inf108">
<mml:math id="m126">
<mml:mrow>
<mml:msub>
<mml:mi>m</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">5.1 &#xd7; 10<sup>6</sup>&#xa0;[kg]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf109">
<mml:math id="m127">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">7.2 &#xd7; 10<sup>8</sup>&#xa0;[N/m]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf110">
<mml:math id="m128">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">5.5 &#xd7; 10<sup>7</sup>&#xa0;[N/m]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf111">
<mml:math id="m129">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mi>I</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">2.2 &#xd7; 10<sup>7</sup>&#xa0;[N/(m/s)]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf112">
<mml:math id="m130">
<mml:mrow>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.0195&#xa0;[m]</td>
</tr>
<tr>
<td rowspan="3" colspan="2" align="left">SDOF</td>
<td align="center">
<inline-formula id="inf113">
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<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mi>e</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">6.7 &#xd7; 10<sup>7</sup>&#xa0;[kg]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf114">
<mml:math id="m132">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">2.1 &#xd7; 10<sup>8</sup>&#xa0;[N/m]</td>
</tr>
<tr>
<td align="center">
<inline-formula id="inf115">
<mml:math id="m133">
<mml:mrow>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.0676&#xa0;[m]</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>Since the second stiffness <inline-formula id="inf116">
<mml:math id="m134">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the damping coefficient <inline-formula id="inf117">
<mml:math id="m135">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model after yielding in the base-isolation story are computed iteratively, those values change depending on the input velocity level of the critical double impulse. The relations of <inline-formula id="inf118">
<mml:math id="m136">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf119">
<mml:math id="m137">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> with the input velocity <inline-formula id="inf120">
<mml:math id="m138">
<mml:mi>V</mml:mi>
</mml:math>
</inline-formula> are shown in <xref ref-type="fig" rid="F6">Figures 6A,B</xref>. It can be observed that, as <inline-formula id="inf121">
<mml:math id="m139">
<mml:mi>V</mml:mi>
</mml:math>
</inline-formula> increases and the plastic deformation becomes larger, the second stiffness <inline-formula id="inf122">
<mml:math id="m140">
<mml:mrow>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mi>e</mml:mi>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the damping coefficient <inline-formula id="inf123">
<mml:math id="m141">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the SDOF model become larger and those values converge to constant values finally. It should be remarked that, while the damping coefficient <inline-formula id="inf124">
<mml:math id="m142">
<mml:mrow>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is constant at the lower level around 0.7 &#xd7; 10<sup>7</sup>&#xa0;(N/(m/s)) in the previous method (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>; <xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>), the proposed method provides a larger value depending on the input velocity level. <xref ref-type="fig" rid="F6">Figure&#x20;6C</xref> indicates the maximum deformation comparison of the base-isolation story among the proposed one, the 2DOF model under the one-cycle sine wave, the plane frame under the one-cycle sine wave, and the previous one by <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref>. It can be seen that, while the previous method (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>) exhibits an inaccurate result, especially for a larger input level due to the factors explained in <xref ref-type="fig" rid="F6">Figure&#x20;6B</xref> (the estimation of a smaller damping coefficient for the SDOF model), the proposed method for the SDOF model can evaluate the maximum deformation of the base-isolation story of the plane frame accurately. In addition, it is noted that the present model employs a bilinear hysteretic restoring-force model (second stiffness ratio &#x3d; 0.077) for the base-isolation story while an elastic-perfectly plastic model was used in the previous method mentioned above. This may slightly affect the difference in <xref ref-type="fig" rid="F6">Figure&#x20;6C</xref>.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Parameters of reduced SDOF model with respect to input velocity level and accuracy check of proposed simple response evaluation method for SDOF model with respect to input velocity level, <bold>(A)</bold> Second-branch stiffness of SDOF model, <bold>(B)</bold> Damping coefficient, <bold>(C)</bold> Maximum deformation comparison of base-isolation story among proposed one, 2DOF model under one-cycle sine wave, plane frame under one-cycle sine wave and previous work by <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref>.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g006.tif"/>
</fig>
</sec>
</sec>
<sec id="s5">
<title>5 A Simple Critical Response Evaluation Method for Base-Isolation Building-Connection Hybrid System Under Double Impulse as Representative of Near-Fault Ground Motion</title>
<p>Consider a base-isolation, building-connection hybrid control system as shown in <xref ref-type="fig" rid="F7">Figure&#x20;7</xref>. By extending the previous method by <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> to a more sophisticated method including an accurate damping evaluation, a more reliable response evaluation method for a simple SDOF model is presented. This method enables the evaluation of the maximum deformation of the base-isolation story under a double impulse as a representative of near-fault ground motions without laborious time-history response analysis.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Plane frame including base-isolation building-connection hybrid control system and its reduction to SDOF model supported on rigid wall by compensated oil dampers.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g007.tif"/>
</fig>
<sec id="s5-1">
<title>5.1&#x20;Base-Isolation Building-Connection Hybrid System</title>
<p>The member parameters of this system are the same as those in <xref ref-type="table" rid="T1">Table&#x20;1</xref>. The connection dampers are placed on stories 4, 8, 12, 16, 18, 20, 22, 24, and 26. While <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> treated a shear building model, the present paper deals with a reinforced concrete plane frame. As in <xref ref-type="sec" rid="s4-1">Section 4.1</xref>, the structural damping ratio of the super-structure (instantaneous stiffness-proportional damping) is set to 0.03. The strength of concrete is Fc60 (60&#xa0;[N/mm<sup>2</sup>]) and the Young&#x2019;s modulus is 33,500&#xa0;[N/mm<sup>2</sup>]. In addition, the restoring-force characteristic of the base-isolation story is extended from the elastic-perfectly plastic model to the bilinear hysteretic model for the purpose of practicality.</p>
</sec>
<sec id="s5-2">
<title>5.2 Transformation of Base-Isolation Building-Connection Hybrid System into SDOF Model</title>
<p>The simplified SDOF model of a base-isolated building is further reduced to another SDOF model by connecting that SDOF model to a rigid wall as a representative of a stiff sub-building as shown in <xref ref-type="fig" rid="F7">Figure&#x20;7</xref>. In this simplification procedure, a compensation coefficient <inline-formula id="inf125">
<mml:math id="m143">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for connecting dampers is introduced as in the method of <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref> to include 1) the effect of rigid modeling of the sub building for simple treatment, 2) the effect of the location of connecting dampers, and 3) the effect of height of the sub building. The novel point is in the damping evaluation in the simplification of the base-isolated building explained in <xref ref-type="sec" rid="s4">Section&#x20;4</xref>.</p>
<p>As in the method by <xref ref-type="bibr" rid="B13">Hayashi (2018)</xref>, the RMDOF model with the compensation factor <inline-formula id="inf126">
<mml:math id="m144">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the connecting dampers is considered as shown in <xref ref-type="fig" rid="F8">Figure&#x20;8A</xref> to reflect the above three factors (rigid modeling of sub building, location of connecting dampers, height of the sub building).</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Introduction of RMDOF model and procedure for evaluating compensation factor <inline-formula id="inf127">
<mml:math id="m145">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(A)</bold> MDOF plane frame model with hybrid control system and RMDOF plane frame model, <bold>(B)</bold> Procedure for evaluating compensation factor <inline-formula id="inf128">
<mml:math id="m146">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> without repetition.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g008.tif"/>
</fig>
<p>The compensation factor <inline-formula id="inf129">
<mml:math id="m147">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> for the connecting dampers is determined so that the lowest damping ratio <inline-formula id="inf130">
<mml:math id="m148">
<mml:mrow>
<mml:msub>
<mml:mi>h</mml:mi>
<mml:mi>R</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (by complex eigenvalue analysis) of the RMDOF model coincides with that <inline-formula id="inf131">
<mml:math id="m149">
<mml:mrow>
<mml:msub>
<mml:mi>h</mml:mi>
<mml:mi>M</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> of the hybrid-controlled plane building frame.<disp-formula id="e19">
<mml:math id="m150">
<mml:mrow>
<mml:msub>
<mml:mi>h</mml:mi>
<mml:mi>M</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>h</mml:mi>
<mml:mi>R</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(19)</label>
</disp-formula>
</p>
<p>
<xref ref-type="disp-formula" rid="e19">Equation 19</xref> requires repetition for obtaining <inline-formula id="inf132">
<mml:math id="m151">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. To avoid this repetition, it is assumed that <inline-formula id="inf133">
<mml:math id="m152">
<mml:mrow>
<mml:msub>
<mml:mi>h</mml:mi>
<mml:mi>R</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is linear to the total damper quantity. Let <inline-formula id="inf134">
<mml:math id="m153">
<mml:mrow>
<mml:msubsup>
<mml:mi>h</mml:mi>
<mml:mi>R</mml:mi>
<mml:mo>&#x2217;</mml:mo>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> denote the lowest damping ratio of the RMDOF model with the original total damper quantity <inline-formula id="inf135">
<mml:math id="m154">
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mo>&#xd7;</mml:mo>
<mml:msub>
<mml:mi>n</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> as shown in <xref ref-type="fig" rid="F8">Figure&#x20;8B</xref>.</p>
<p>In the complex eigenvalue analysis, it is necessary to determine the equivalent stiffness of the base-isolation story. In this paper, the equivalent stiffness is to be obtained from the analysis for the SDOF model with <inline-formula id="inf136">
<mml:math id="m155">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> (initial assumption) where the equivalent stiffness of the base-isolation story is evaluated using the 2DOF model. While the Hayashi&#x2019;s model and method (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>) requires repetition for evaluating <inline-formula id="inf137">
<mml:math id="m156">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> due to the inaccuracy in the evaluation of the equivalent damping coefficient, the proposed method highly enhances the reliability and accuracy because of the upgrade of the accuracy in the response evaluation in terms of the SDOF&#x20;model.</p>
<p>
<xref ref-type="fig" rid="F9">Figure&#x20;9A</xref> shows the relation of the lowest-mode damping&#x20;ratio of the MDOF model and the RMDOF model&#x20;with the equivalent stiffness of the base-isolation story where five damping coefficients of the connecting damper are taken. The following observation can be drawn from <xref ref-type="fig" rid="F9">Figure&#x20;9A</xref>
<list list-type="simple">
<list-item>
<p>&#x2a;The lowest-mode damping ratio of the MDOF model exhibits different values depending on the equivalent stiffness. The variation is large in the range of smaller equivalent stiffness.</p>
</list-item>
<list-item>
<p>&#x2a;The lowest-mode damping ratio of the RMDOF model indicates larger values than the MDOF model. The difference is larger in the range of larger equivalent stiffness.</p>
</list-item>
</list>
</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Evaluation of compensation factor, <bold>(A)</bold> Relation of lowest-mode damping ratio of MDOF model and RMDOF model with equivalent stiffness of base-isolation story where five damping coefficients of connecting damper, <bold>(B)</bold> Relation of equivalent stiffness of base-isolation story with input velocity level, <bold>(C)</bold> Relation of compensation factor with input velocity&#x20;level.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g009.tif"/>
</fig>
<p>Once such a relationship is obtained, the compensation factor <inline-formula id="inf138">
<mml:math id="m157">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> can be determined by using the equivalent stiffness corresponding to the input velocity level. <xref ref-type="fig" rid="F9">Figures 9B,C</xref> present the relation of the equivalent stiffness of the base-isolation story with the input velocity level and the relation of the compensation factor with the input velocity level. It can be observed from <xref ref-type="fig" rid="F9">Figures 9B,C</xref> that, as the damping coefficients of connecting dampers becomes large, the compensation factor becomes smaller for a smaller input velocity level. It is noted that only eigenvalue analysis is needed for MDOF and RMDOF models and the response evaluation is conducted only for the SDOF model by using the closed-form expression (<xref ref-type="bibr" rid="B1">Akehashi et&#x20;al., 2018</xref>).</p>
<p>
<xref ref-type="fig" rid="F10">Figure&#x20;10</xref> presents the comparison of the maximum deformation of the base-isolation story by the proposed method for the SDOF model (with and without compensation factor) with that by time-history response analysis for the plane frame model for various connection damper levels. It can be observed that, while the proposed method exhibits a good correspondence to the plane frame model regardless of the compensation factor <inline-formula id="inf139">
<mml:math id="m158">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> in the small connection damper level, the compensation factor plays an important role in the larger connection damper level. It seems that this results from the fact that, when the connection damper level becomes larger, the effect of the assumption of the rigid sub-building arises strongly. This fact can also be understood from the result that, as the connection damper level becomes larger, <inline-formula id="inf140">
<mml:math id="m159">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b2;</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> becomes smaller (see <xref ref-type="fig" rid="F9">Figure&#x20;9C</xref>). This indicates the compensation effect clearly.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>Comparison of the maximum deformation of the base-isolation story by the proposed method for the SDOF model (with and without compensation factor) with that by time-history response analysis for the plane frame model for various connection damper levels, <bold>(A)</bold> <inline-formula id="inf141">
<mml:math id="m160">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.208&#xa0;[kN/(mm/s)], <bold>(B)</bold> <inline-formula id="inf142">
<mml:math id="m161">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.417&#xa0;[kN/(mm/s)], <bold>(C)</bold> <inline-formula id="inf143">
<mml:math id="m162">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.521&#xa0;[kN/(mm/s)], <bold>(D)</bold> <inline-formula id="inf144">
<mml:math id="m163">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.625&#xa0;[kN/(mm/s)], <bold>(E)</bold> <inline-formula id="inf145">
<mml:math id="m164">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.833&#xa0;[kN/(mm/s)].</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g010.tif"/>
</fig>
</sec>
</sec>
<sec id="s6">
<title>6 Verification of Validity of Using One-Cycle Sine Wave Equivalent to Critical Double Impulse for SDOF Model as Critical Input for Plane Frame</title>
<p>In <xref ref-type="sec" rid="s4">Sections 4</xref>, <xref ref-type="sec" rid="s5">5</xref>, the one-cycle sine wave equivalent to the critical double impulse for the SDOF model was used to verify the accuracy of the proposed response evaluation method. However, it seems necessary to check whether the critical double impulse for the SDOF model is actually critical for the plane frame model. In this section, this issue will be investigated.</p>
<sec id="s6-1">
<title>6.1 Critical Double Impulse for Plane Frame</title>
<p>Recently, many multi-purpose structural analysis programs have become available. In this paper, a general-purpose structural analysis program SNAP (<xref ref-type="bibr" rid="B25">Kozo System Co., 2019</xref>) is used. In this program, the accuracy check is included automatically, e.g., the processing of unbalanced forces.</p>
<p>The double impulse <inline-formula id="inf146">
<mml:math id="m165">
<mml:mrow>
<mml:msubsup>
<mml:mrow>
<mml:mover accent="true">
<mml:mi>u</mml:mi>
<mml:mo>&#xa8;</mml:mo>
</mml:mover>
</mml:mrow>
<mml:mi>g</mml:mi>
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> is to be expressed by a one-point (triangular) acceleration input <inline-formula id="inf147">
<mml:math id="m166">
<mml:mrow>
<mml:msubsup>
<mml:mrow>
<mml:mover accent="true">
<mml:mi>u</mml:mi>
<mml:mo>&#xa8;</mml:mo>
</mml:mover>
</mml:mrow>
<mml:mi>g</mml:mi>
<mml:mrow>
<mml:mi>T</mml:mi>
<mml:mi>R</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> where the triangle area of this input corresponds to the impulse <inline-formula id="inf148">
<mml:math id="m167">
<mml:mrow>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>N</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>. This relation can be expressed by<disp-formula id="e20">
<mml:math id="m168">
<mml:mrow>
<mml:msub>
<mml:mi>A</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>N</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mi>&#x394;</mml:mi>
<mml:mi>t</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>I</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>N</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(20)</label>
</disp-formula>
</p>
<p>
<xref ref-type="bibr" rid="B20">Kawai et&#x20;al. (2021)</xref> showed that <inline-formula id="inf149">
<mml:math id="m169">
<mml:mrow>
<mml:mi>&#x394;</mml:mi>
<mml:mi>t</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.01</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> [s] is sufficient enough for the accuracy. It is noted that, since a rapid change of input acceleration may cause the occurrence of unbalanced forces, division of the time interval into short durations is often conducted.</p>
<p>Furthermore, <xref ref-type="bibr" rid="B2">Akehashi and Takewaki (2019)</xref> made clear that the critical input of the second impulse can be characterized by the criterion that the critical timing of the second impulse is the time of the zero story shear in the first story. For the present model, the following relation holds.<disp-formula id="e21">
<mml:math id="m170">
<mml:mrow>
<mml:mi>F</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msubsup>
<mml:mi>F</mml:mi>
<mml:mi>M</mml:mi>
<mml:mn>1</mml:mn>
</mml:msubsup>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>F</mml:mi>
<mml:mi>F</mml:mi>
<mml:mn>1</mml:mn>
</mml:msubsup>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
<label>(21)</label>
</disp-formula>where <inline-formula id="inf150">
<mml:math id="m171">
<mml:mrow>
<mml:msubsup>
<mml:mi>F</mml:mi>
<mml:mi>M</mml:mi>
<mml:mn>1</mml:mn>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> is the base-isolation story shear force of the main building and <inline-formula id="inf151">
<mml:math id="m172">
<mml:mrow>
<mml:msubsup>
<mml:mi>F</mml:mi>
<mml:mi>F</mml:mi>
<mml:mn>1</mml:mn>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula> is the first-story shear force of the sub building. <xref ref-type="fig" rid="F11">Figure&#x20;11</xref> shows the critical timing of the second impulse and the simulation of the impulses by one-point (triangular) acceleration inputs.</p>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>Critical timing of second impulse and simulation of impulse by one-point acceleration&#x20;input.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g011.tif"/>
</fig>
</sec>
<sec id="s6-2">
<title>6.2 Comparison of the Response of Plane Frame to One-Cycle Sine Wave With Response to Impulsive Acceleration Input</title>
<p>
<xref ref-type="fig" rid="F12">Figure&#x20;12A</xref> shows the comparison of the maximum deformation of the base-isolation story of the plane frame model under the one-cycle sine wave equivalent to the critical double impulse for the SDOF model with that under the critical double impulse (a pair of inverse-direction one-point acceleration inputs) for the plane frame model. The connection damping coefficient is given by <inline-formula id="inf152">
<mml:math id="m173">
<mml:mi>c</mml:mi>
</mml:math>
</inline-formula> &#x3d; 0.417&#xa0;[kN/(mm/s)] and the time increment is specified as <inline-formula id="inf153">
<mml:math id="m174">
<mml:mrow>
<mml:mi>&#x394;</mml:mi>
<mml:mi>t</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.01</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> [s]. It can be observed that both plots correspond well. This indicates the reliability and accuracy of using the SDOF model and the critical double impulse for the SDOF&#x20;model.</p>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>Comparison of deformation of the base-isolation story of plane frame model under one-cycle sine wave equivalent to the critical double impulse for SDOF model with that under critical double impulse (a pair of inverse-direction one-point acceleration inputs) for plane frame model, <bold>(A)</bold> Maximum deformation of base-isolation story, <bold>(B)</bold> Time history of deformation of the base-isolation story (input velocity level <italic>V</italic>&#x20;&#x3d; 1.0&#xa0;[m/s]).</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g012.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F12">Figure&#x20;12B</xref> illustrates the time histories of the above-mentioned two inputs. The phases of the time histories are adjusted. It can be understood that the responses under both inputs coincide well and the simple response evaluation method proposed in the paper is reliable.</p>
</sec>
</sec>
<sec id="s7">
<title>7 Investigation on Performance of Proposed Evaluation Method Through Time-History Response Analysis for Recorded Ground Motion</title>
<p>It seems important to demonstrate the applicability of the proposed simple response evaluation method to actual recorded ground motions.</p>
<p>
<xref ref-type="fig" rid="F13">Figure&#x20;13</xref> shows the applicability of the proposed evaluation method to a recorded ground motion through the time-history response analysis (Rinaldi Station FN comp. during1994 Northridge). <xref ref-type="fig" rid="F13">Figure&#x20;13A</xref> presents the recorded ground motion acceleration and the corresponding one-cycle sinusoidal wave where the acceleration amplitude and the period of the extracted one-cycle sinusoidal wave are 7.85&#xa0;[m/s] and 0.8&#xa0;[s]. As for connecting dampers, the damping coefficient <italic>c</italic>&#x20;&#x3d; 2.5 &#xd7; 10<sup>6</sup>&#xa0;[Ns/m] is used. The other parameters are the same as in the previous section. <xref ref-type="fig" rid="F13">Figure&#x20;13B</xref> illustrates the maximum displacement of the SDOF model by the proposed method under the critical double impulse and by the time-history response analysis under the recorded ground motion. Since the amplitude and the period of the one-cycle sinusoidal wave are fixed, the model parameters <inline-formula id="inf154">
<mml:math id="m175">
<mml:mrow>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> are changed with the relation <inline-formula id="inf155">
<mml:math id="m176">
<mml:mrow>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
<mml:msub>
<mml:mi>d</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> where <inline-formula id="inf156">
<mml:math id="m177">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c9;</mml:mi>
<mml:mn>1</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the elastic natural circular frequency and <italic>d<sub>ye</sub>
</italic> is the elastic limit deformation of the SDOF model. This procedure may be similar to the work by <xref ref-type="bibr" rid="B45">Veletsos et&#x20;al. (1965)</xref> for the inelastic response spectrum where the yield displacement or yield strength is changed to attain the specified ductility factor. It can be observed that the proposed method exhibits an accurate result. <xref ref-type="fig" rid="F13">Figure&#x20;13C</xref> shows the time-history response for the SDOF model under the critical double impulse corresponding to the one-cycle sinusoidal wave and the recorded ground motion for the input velocity level <inline-formula id="inf157">
<mml:math id="m178">
<mml:mrow>
<mml:mi>V</mml:mi>
<mml:mo>/</mml:mo>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>4.19</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>. It can be seen that the maximum displacement exhibits a good correspondence.</p>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>Comparison of proposed evaluation method with time-history response analysis for recorded ground motion, <bold>(A)</bold> Rinaldi Station FN comp. (1994 Northridge) and one-cycle sinusoidal wave, <bold>(B)</bold> Maximum displacement of SDOF model by the proposed method under critical double impulse and by time-history response analysis under recorded ground motion, <bold>(C)</bold> Time-history response analysis for SDOF model under critical double impulse and recorded ground motion for <inline-formula id="inf158">
<mml:math id="m179">
<mml:mrow>
<mml:mrow>
<mml:mi>V</mml:mi>
<mml:mo>/</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>4.19</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fbuil-07-790584-g013.tif"/>
</fig>
</sec>
<sec id="s8">
<title>8 Conclusion</title>
<p>An innovative building system including a base-isolation, building-connection hybrid control system proposed in the previous study has been revisited. This building system has advantageous features to withstand pulse-type earthquake ground motions through the base-isolation system and to resist long-duration earthquake ground motions through the building-connection system.<list list-type="simple">
<list-item>
<p>1) While the previous response evaluation method with an amplitude-narrow-band damping evaluation procedure exhibited a rather inaccurate result, a simple and more accurate response evaluation method without nonlinear time-history response analysis has been proposed for this hybrid-controlled building system under near-fault ground motions.</p>
</list-item>
<list-item>
<p>2) It was demonstrated that the previously derived analytical expression of the elastic-plastic deformation of a bilinear hysteretic single-degree-of-freedom (SDOF) model with lead rubber isolators and oil dampers can be used effectively under the double impulse as a representative of pulse-type ground motions.</p>
</list-item>
<list-item>
<p>3) A two-step transformation from this innovative hybrid structural system into an SDOF model via a 2DOF model has been proposed. The first step is the transformation of the main base-isolated building into an SDOF system via a 2DOF model and the second step is the reduction of the connecting oil dampers supported on a sub building to upper-story concentrated oil dampers with a revised compensation factor on a rigid wall. The compensation factor reflects 1) the effect of rigid modeling of the sub building, 2) the effect of the location of connecting dampers, 3) the effect of height of the sub building.</p>
</list-item>
<list-item>
<p>4) It was made clear that the evaluation of damping coefficients is a key step in the upgrade of accuracy. Different from the previous work (<xref ref-type="bibr" rid="B13">Hayashi, 2018</xref>; <xref ref-type="bibr" rid="B12">Hayashi et&#x20;al., 2018</xref>), the equivalent damping coefficient was obtained depending on the response range before and after yielding. Effective use of the closed-form expression of the elastic-plastic deformation to the reduced SDOF model enables the development of a simple and sophisticated response evaluation method.</p>
</list-item>
<list-item>
<p>5) The time-history response analysis of the plane frame model under the critical double impulse and a one-cycle sine wave equivalent to the critical double impulse for an SDOF model demonstrated the accuracy of the proposed response evaluation method.</p>
</list-item>
<list-item>
<p>6) It was demonstrated that the proposed method exhibits a reliable performance for recorded ground motions.</p>
</list-item>
</list>
</p>
<p>The behavior of the sub-building seems to influence the total response of this base-isolation, building-connection hybrid control system because the sub-building is usually made of reinforced-concrete wall structures whose structural properties have never been made clear. The reflection of this property on the total response evaluation system will be desired for a more accurate and reliable design.</p>
</sec>
</body>
<back>
<sec id="s9">
<title>Data Availability Statement</title>
<p>The raw data supporting the conclusion of this article will be made available by the authors, without undue reservation.</p>
</sec>
<sec id="s10">
<title>Author Contributions</title>
<p>TN formulated the problem, conducted the computation, and&#x20;wrote the paper. KF conducted the computation and discussed the results. IT supervised the research and wrote the paper.</p>
</sec>
<sec id="s11">
<title>Funding</title>
<p>Part of the present work is supported by the JSPS KAKENHI (No. 18H01584). This support is greatly appreciated.</p>
</sec>
<sec sec-type="COI-statement" id="s12">
<title>Conflict of Interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
<sec sec-type="disclaimer" id="s13">
<title>Publisher&#x2019;s Note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
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