<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article PUBLIC "-//NLM//DTD JATS (Z39.96) Journal Publishing DTD v1.3 20210610//EN" "https://jats.nlm.nih.gov/publishing/1.3/JATS-journalpublishing1-3.dtd"><article xml:lang="en" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:ali="http://www.niso.org/schemas/ali/1.0/" dtd-version="1.3" article-type="research-article"><front><journal-meta><journal-id journal-id-type="issn">2460-0245</journal-id><journal-title-group><journal-title>Journal of the Indonesian Mathematical Society</journal-title><abbrev-journal-title>JIMS</abbrev-journal-title></journal-title-group><issn pub-type="epub">2460-0245</issn><issn pub-type="ppub">2086-8952</issn><publisher><publisher-name>IndoMS</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.22342/jims.v32i3.1709</article-id><article-categories></article-categories><title-group><article-title>Analysis of Primary Resonance in Damped Duffing-Helmholtz Oscillator Excited by an Amplitude-Modulated Signal</article-title></title-group><contrib-group><contrib contrib-type="author"><name><surname>Kumar</surname><given-names>Chaudhary Anunay</given-names></name><address><country country="IN">India</country><email>akchaudhary@svc.ac.in</email></address><xref ref-type="aff" rid="AFF-1"></xref></contrib><contrib contrib-type="author"><name><surname>Saureesh</surname><given-names>Das</given-names></name><address><country country="IN">India</country><email>saureeshdas@gmail.com</email></address><xref ref-type="aff" rid="AFF-2"></xref></contrib><contrib contrib-type="author"><name><surname>Pankaj</surname><given-names>Narang</given-names></name><address><country country="IN">India</country><email>pnarang@arsd.du.ac.in</email></address><xref ref-type="aff" rid="AFF-3"></xref></contrib><contrib contrib-type="author"><name><surname>Kanti</surname><given-names>Das Mrinal</given-names></name><address><country country="IN">India</country><email>dasmkd11@gmail.com</email></address><xref ref-type="aff" rid="AFF-4"></xref><xref ref-type="corresp" rid="cor-0"></xref></contrib></contrib-group><contrib-group><contrib contrib-type="editor"><name><surname>Rizal</surname><given-names>Jose</given-names></name><address><email>jrizal04@unib.ac.id</email></address></contrib></contrib-group><aff id="AFF-1"><institution content-type="dept">Sri Venkateswara College</institution><institution-wrap><institution>University of Delhi South Campus</institution><institution-id institution-id-type="ror">https://ror.org/04gzb2213</institution-id></institution-wrap><country country="IN">India</country></aff><aff id="AFF-2"><institution content-type="dept">Institute of Informatics and Communication</institution><institution-wrap><institution>University of Delhi</institution><institution-id institution-id-type="ror">https://ror.org/04gzb2213</institution-id></institution-wrap><country country="IN">India</country></aff><aff id="AFF-3"><institution content-type="dept">A. R. S. D. College</institution><institution-wrap><institution>University of Delhi South Campus</institution><institution-id institution-id-type="ror">https://ror.org/04gzb2213</institution-id></institution-wrap><country country="IN">India</country></aff><aff id="AFF-4"><institution content-type="dept">Institute of Informatics and Communication</institution><institution-wrap><institution>University of Delhi South Campus</institution><institution-id institution-id-type="ror">https://ror.org/04gzb2213</institution-id></institution-wrap><country country="IN">India</country></aff><author-notes><fn fn-type="coi-statement"><label>Conflicts of Interest.</label><p>Authors declare that they do not have any known conflict of interest.</p></fn><corresp id="cor-0">Corresponding author: Das Mrinal Kanti. Email: <email>dasmkd11@gmail.com</email></corresp></author-notes><pub-date date-type="pub" iso-8601-date="2026-09-01" publication-format="electronic"><day>01</day><month>09</month><year>2026</year></pub-date><pub-date date-type="collection" iso-8601-date="2026-09-01" publication-format="electronic"><day>01</day><month>09</month><year>2026</year></pub-date><volume>32</volume><issue>3</issue><issue-title>Vol. 32 No. 3 (2026): SEPTEMBER</issue-title><fpage>1</fpage><lpage>14</lpage><history><date date-type="received" iso-8601-date="2024-05-20"><day>20</day><month>05</month><year>2024</year></date><date date-type="accepted" iso-8601-date="2026-03-01"><day>01</day><month>03</month><year>2026</year></date></history><permissions><copyright-statement>Copyright (c) 2026 Journal of the Indonesian Mathematical Society</copyright-statement><copyright-year>2026</copyright-year><copyright-holder>Journal of the Indonesian Mathematical Society</copyright-holder><license xlink:href="https://creativecommons.org/licenses/by-nc-nd/4.0/"><ali:license_ref xmlns:ali="http://www.niso.org/schemas/ali/1.0/">https://creativecommons.org/licenses/by-nc-nd/4.0/</ali:license_ref><license-p>This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.</license-p></license></permissions><self-uri xlink:href="https://jims-a.org/index.php/jimsa/article/view/1709" xlink:title="1709"></self-uri><abstract><p>The effect of amplitude modulated signal on the primary resonance on a Duffing-Helmholtz oscillator has been investigated using (<italic>i</italic>) a multiple time scale perturbation method involving two different time scales i.e., regular time (T 0 ) and a slow time, (<inline-formula><tex-math id="math-1"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle T_1 \end{document} ]]></tex-math></inline-formula>), to analyze the system response and (<italic>ii</italic>) its modified version which is valid for larger values of expansion parameter viz., asymptotic ordering parameter, incorporating Lindstedt-Poincare transformation method that allows the interaction of the amplitude and frequency of the response. The modification of the amplitude-frequency plots, exhibiting bi-stable behavior, caused by different values of modulation amplitude and damping has been obtained both analytically and numerically for various parameters of the system near the primary resonance. The peak amplitude of the response is shown to get lowered in strongly nonlinear Duffing-type system. Phase plane trajectories of stable and unstable manifolds are presented in different instances.</p></abstract><kwd-group><kwd>Duffing-Helmholtz oscillator</kwd><kwd>bi-stability</kwd><kwd>amplitude modulation</kwd><kwd>primary and secondary resonance</kwd><kwd>stable and unstable manifolds</kwd></kwd-group><funding-group><funding-statement>The authors declare that no financial support was received for this research, authorship, and publication of this article.</funding-statement></funding-group><custom-meta-group><custom-meta><meta-name>File created by JATS Editor</meta-name><meta-value>https://jatseditor.com</meta-value></custom-meta><custom-meta><meta-name>issue-created-year</meta-name><meta-value>2026</meta-value></custom-meta></custom-meta-group></article-meta></front><body><sec id="sec-1"><title>1. INTRODUCTION</title><p>Oscillators comprising of both cubic and quadratic nonlinear terms are termed in Kovacic and Gatti <xref ref-type="bibr" rid="BIBR-1">[1]</xref> as Dufing-Helmholtz oscillators. In case of a linear damped system with displacement, Q(t), we may represent Dufing-Helmholtz system as:</p><disp-formula id="equation-1"><tex-math id="math-2"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \ddot {Q} + 2 \mu_ {0} \dot {Q} + \omega_ {0} ^ {2} Q + I _ {1} Q ^ {2} + I _ {2} Q ^ {3} = 0,\tag{1} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-3"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mu _ { 0 } , \omega _ { 0 } , I _ { 1 } \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-4"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } \end{document} ]]></tex-math></inline-formula> refer the linear damping coeficient, the natural frequency, strength of quadratic and cubic non-linearities of the system, respectively. It may be noted that, for the presence of only quadratic non-linearity, i.e. <inline-formula><tex-math id="math-5"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } = 0 . \end{document} ]]></tex-math></inline-formula> , equation (1) represents a Helmholtz asymmetric oscillator as in Kovacic and Brennan <xref ref-type="bibr" rid="BIBR-2">[2]</xref> while in the absence of the quadratic nonlinear term i.e., <inline-formula><tex-math id="math-6"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 1 } = 0 , \end{document} ]]></tex-math></inline-formula> , equation (1) refers to the Dufing type oscillator used earlier to study pendulum dynamics with cubic nonlinear restoring term (Kovacic and Gatti <xref ref-type="bibr" rid="BIBR-1">[1]</xref>). The application of Cardano’s transformation i.e., <inline-formula><tex-math id="math-7"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { q ( t ) = Q ( t ) + \frac { I _ { 1 } } { 3 I _ { 2 } } } \end{array} \end{document} ]]></tex-math></inline-formula> allows one to write the Dufing-Helmholtz system (1.1) as a Dufing type oscillator,</p><disp-formula id="equation-2"><tex-math id="math-8"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \ddot {q} + 2 \mu_ {0} \dot {q} + \Omega_ {0} ^ {2} q + I _ {2} q ^ {3} = f - k _ {0},\tag{2} \end{document} ]]></tex-math></disp-formula><p>with <inline-formula><tex-math id="math-9"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { \Omega _ { 0 } ^ { 2 } \ = \ \omega _ { 0 } ^ { 2 } \ - \ \frac { I _ { 1 } ^ { 2 } } { 3 I _ { 2 } } } \end{array} \end{document} ]]></tex-math></inline-formula> defining the transformed natural frequency of the system, <inline-formula><tex-math id="math-10"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { k _ { 0 } = \frac { 2 I _ { 1 } ^ { 3 } } { 2 7 I _ { 2 } ^ { 2 } } - \omega _ { 0 } ^ { 2 } \frac { I _ { 1 } } { 3 I _ { 2 } } } \end{array} \end{document} ]]></tex-math></inline-formula> is a constant and may be considered as a steady bias for the oscillator as in Das <xref ref-type="bibr" rid="BIBR-3">[3]</xref> and f is the time dependent excitation that controls the dynamics externally (Mallik <xref ref-type="bibr" rid="BIBR-4">[4]</xref>). Various instances of the Dufing type oscillator and synchronization of coupled oscillators have been investigated earlier, both analytically and numerically in Bhardwaj and Das <xref ref-type="bibr" rid="BIBR-5">[5]</xref>, Mickens <xref ref-type="bibr" rid="BIBR-6">[6]</xref> and Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref> and, in recent years in Brennan and Kovacic <xref ref-type="bibr" rid="BIBR-8">[8]</xref>, Chen, et.al. <xref ref-type="bibr" rid="BIBR-9">[9]</xref>, Das and Bhardwaj <xref ref-type="bibr" rid="BIBR-10">[10]</xref>, Das <xref ref-type="bibr" rid="BIBR-3">[3]</xref>, Kalm´ar-Nagy and Balachandran <xref ref-type="bibr" rid="BIBR-11">[11]</xref>, Lie, et.al. <xref ref-type="bibr" rid="BIBR-12">[12]</xref>, Mickens <xref ref-type="bibr" rid="BIBR-13">[13]</xref>, Ramlan, et.al. <xref ref-type="bibr" rid="BIBR-14">[14]</xref>, WaWrzynski <xref ref-type="bibr" rid="BIBR-15">[15]</xref>, WaWrzynski <xref ref-type="bibr" rid="BIBR-16">[16]</xref>. Among the commonly used tools of nonlinear system analysis (Chaudhary, et.al. <xref ref-type="bibr" rid="BIBR-17">[17]</xref> and Kovacic and Brennan <xref ref-type="bibr" rid="BIBR-18">[18]</xref>) viz., frequency response curve, backbone curve, time histories, phase portraits, bifurcation analysis, Poincare section, basin of attraction, etc., the frequency response curve is commonly used in engineering mechanics to estimate the resonance frequency, jump-up/down frequencies etc. In particular, recently in WaWrzynski <xref ref-type="bibr" rid="BIBR-16">[16]</xref>, the idea of origin point is introduced, based on bistability region and unstable solution domain of the periodically excited Dufing system, to understand its dynamics. Earlier, in Brennan, et.al. <xref ref-type="bibr" rid="BIBR-19">[19]</xref>, Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>, using Harmonic balance method (Mickens <xref ref-type="bibr" rid="BIBR-6">[6]</xref>) wherein a periodic solution is expressed in terms of superposition of sinusoidal functions and multi-scale perturbation analysis involving two time scales, a linearly damped harmonically excited Dufing type system is known to exhibit jump-up frequency as dependent mainly on the nonlinearity parameter, <inline-formula><tex-math id="math-11"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } . \end{document} ]]></tex-math></inline-formula> , whereas the jump-down frequency is ob served to be dependent on both <inline-formula><tex-math id="math-12"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } \end{document} ]]></tex-math></inline-formula> and the damping parameter, <inline-formula><tex-math id="math-13"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mu , \end{document} ]]></tex-math></inline-formula> respectively. The primary aim of the present work is to recast the usual small perturbation method (Mickens <xref ref-type="bibr" rid="BIBR-13">[13]</xref>, Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>) of multiple time scales perturbation method [MTPM] (applicable to only weakly nonlinear forced oscillatory system) to be amenable to investigate the strongly nonlinear oscillator, <inline-formula><tex-math id="math-14"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . , \end{document} ]]></tex-math></inline-formula> , larger values of the nonlinear parameter <inline-formula><tex-math id="math-15"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } . \end{document} ]]></tex-math></inline-formula> , as well. Such a procedure involves (i) defining a new expansion parameter, α as a function of weak nonlinear parameter, ϵ and (ii) the introduction of a frequency de-tuning parameter, <inline-formula><tex-math id="math-16"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma , \end{document} ]]></tex-math></inline-formula> in the squared frequency, <inline-formula><tex-math id="math-17"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega ^ { 2 } \end{document} ]]></tex-math></inline-formula> of the forcing term as in Burton and Rahman <xref ref-type="bibr" rid="BIBR-20">[20]</xref>. Based on the improved/modified method, the efect of more general form of excitation, i.e., amplitude modulated excitation (AME) on the primary and secondary resonance of a linearly damped</p><p>2</p><p>Dufing type system, <inline-formula><tex-math id="math-18"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . \end{document} ]]></tex-math></inline-formula> , equation (2), has been investigated. Using the improved procedure, the amplitude-frequency response curves of Dufing type system when excited by AME, for diferent parameter settings are obtained in case of primary resonance.</p><p>In section II, we briefly outline the method of MTPM applied to weakly nonlinear Dufing type oscillator and its extension for the strongly nonlinear case. The numerical results regarding the efect of AME on the primary resonance both for (i) weakly and (ii) strongly nonlinear oscillator, for diferent values of parameters of the system are discussed. In section III, we present the results of numerical simulation of the response of the system. Appendix further provides some insight into the stability of the system.</p></sec><sec id="sec-2"><title>2. AMPLITUDE MODULATION EXCITATION EFFECT ON PRIMARY RESONANCE OF DUFFING-TYPE OSCILLATOR</title><p>In this section, we consider the forcing function, <inline-formula><tex-math id="math-19"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle f ( t ) \end{document} ]]></tex-math></inline-formula> , of the externally excited Dufing system, equation (2), to be amplitude modulated. Therefore, we write, <inline-formula><tex-math id="math-20"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle f ( t ) \end{document} ]]></tex-math></inline-formula> as (WaWrzynski <xref ref-type="bibr" rid="BIBR-16">[16]</xref>):</p><disp-formula id="equation-3"><tex-math id="math-21"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle { f ( t ) } { = } { \left[ f _ { 1 0 } + 2 g _ { 1 0 } \cos ( \Omega _ { m } t ) \right] \sin ( \Omega t ) , }\tag{3} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-22"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle f _ { 1 0 } \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-23"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle g _ { 1 0 } \end{document} ]]></tex-math></inline-formula> are amplitudes of the external harmonic excitation and modulation with main excitation frequency or carrier frequency, <inline-formula><tex-math id="math-24"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { : } \end{document} ]]></tex-math></inline-formula> , and modulating frequency, <inline-formula><tex-math id="math-25"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { m } . \end{document} ]]></tex-math></inline-formula> , respectively. Since, <inline-formula><tex-math id="math-26"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle 2 \cos ( \Omega _ { m } t ) \sin ( \Omega t ) = \sin ( \Omega + \Omega _ { m } ) t + \sin ( \Omega - \Omega _ { m } ) t \end{document} ]]></tex-math></inline-formula> the AME excitation of the Dufing type system therefore comprises of two additional frequencies, namely, (1) <inline-formula><tex-math id="math-27"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega + \Omega _ { m } \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-28"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle ( 2 ) ~ \Omega - \Omega _ { m } \end{document} ]]></tex-math></inline-formula> besides the main excitation frequency , Ω. Therefore, with increased complexity of excitation, we may write the reduced form of the Dufingtype equation as,</p><disp-formula id="equation-4"><tex-math id="math-29"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \ddot {q} + 2 \mu_ {0} \dot {q} + \Omega_ {0} ^ {2} q + I _ {2} q ^ {3} = - k _ {0} + [ f _ {1 0} + 2 g _ {1 0} \cos (\Omega_ {m} t) ] \sin (\Omega t).\tag{4} \end{document} ]]></tex-math></disp-formula><p>The dynamical response of the AME Dufing type system, <inline-formula><tex-math id="math-30"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . \end{document} ]]></tex-math></inline-formula> , equation (4), is investigated, in the following, using the multi time scale expansion method (Mickens <xref ref-type="bibr" rid="BIBR-13">[13]</xref>, Mickens <xref ref-type="bibr" rid="BIBR-6">[6]</xref>, Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>) for both instances of weak and strong nonlinearity.</p><sec id="sec-3"><title>2.1. Response of the weakly nonlinear AME excited Dufingtype system using Multi Time Scale Perturbation Method.</title><p>In this section, we focus our attention to the comparison of the dynamic response of a forced dynamic system with weak nonlinearity and the corresponding forced linear case. In order to facilitate such a comparison, a small asymptotic ordering parameter, <inline-formula><tex-math id="math-31"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon < < 1 \end{document} ]]></tex-math></inline-formula> , is introduced and rewrite <inline-formula><tex-math id="math-32"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle k _ { 0 } = { \epsilon } k , f _ { 1 0 } = { \epsilon } f _ { 1 } , g _ { 1 0 } = { \epsilon } g _ { 1 } \end{document} ]]></tex-math></inline-formula> and both damping parameter, <inline-formula><tex-math id="math-33"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mu _ { 0 } = \epsilon \mu \end{document} ]]></tex-math></inline-formula> and the nonlinearity parameter as <inline-formula><tex-math id="math-34"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 2 } = \epsilon \mathbf { I } \end{document} ]]></tex-math></inline-formula> in Dufing type equation (4), as</p><disp-formula id="equation-5"><tex-math id="math-35"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \ddot {q} + 2 \epsilon \mu \dot {q} + \Omega_ {0} ^ {2} q + \epsilon \mathrm{I} q ^ {3} = \epsilon \left\{\left[ f _ {1} + 2 g _ {1} \cos (\Omega_ {m} t) \right] \sin (\Omega t) - k \right\},\tag{5} \end{document} ]]></tex-math></disp-formula><p>where besides weak damping, weak non-linearity, AME term, <inline-formula><tex-math id="math-36"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle f \end{document} ]]></tex-math></inline-formula> is also considered to be weak. The foregoing system, in the absence of quadratic nonlinearity, i.e.,</p><p>3</p><p><inline-formula><tex-math id="math-37"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I _ { 1 } = 0 \end{document} ]]></tex-math></inline-formula> appearing in equation (1) and only harmonically excited Dufing system has been investigated earlier in Chen, <ext-link ext-link-type="uri" xlink:href="https://et.al" xlink:title="et.al">et.al</ext-link>. <xref ref-type="bibr" rid="BIBR-9">[9]</xref>.</p><p>In order to obtain the solution for the case of weak forcing, weak damping and weakly nonlinear Dufing type equation (5) we define (Mickens <xref ref-type="bibr" rid="BIBR-13">[13]</xref>, Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>),</p><disp-formula id="equation-6"><tex-math id="math-38"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm{T} _ {n} = \epsilon^ {n} t \text {with} n = 0, 1, 2, \dots .\tag{6} \end{document} ]]></tex-math></disp-formula><p>Therefore, the derivative with respect to t is now written as expansion in terms of partial derivative with respect to <inline-formula><tex-math id="math-39"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm { T } _ { n } \end{document} ]]></tex-math></inline-formula> and hence, we have</p><disp-formula id="equation-7"><tex-math id="math-40"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \frac {d}{d t} = \frac {\partial}{\partial \mathrm{T} _ {0}} + \epsilon \frac {\partial}{\partial \mathrm{T} _ {1}} + \dots = D _ {0} + \epsilon D _ {1} + \dots \text {and} \frac {d ^ {2}}{d t ^ {2}} = D _ {0} ^ {2} + 2 \epsilon D _ {0} D _ {1} + \dots\tag{7} \end{document} ]]></tex-math></disp-formula><p>where expansions are taken up to <inline-formula><tex-math id="math-41"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle { \mathrm { O } } ( \epsilon ^ { 1 } ) \end{document} ]]></tex-math></inline-formula></p><p>Let the solution of equation (5) be represented in terms of perturbation parameter ϵ as</p><disp-formula id="equation-8"><tex-math id="math-42"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle q (\mathrm{T}; \epsilon) = q _ {0} (\mathrm{T} _ {0}, \mathrm{T} _ {1}) + \epsilon q _ {1} (\mathrm{T} _ {0}, \mathrm{T} _ {1}, \dots) + \dots .\tag{8} \end{document} ]]></tex-math></disp-formula><p>Substituting for <inline-formula><tex-math id="math-43"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle q ( \mathrm { T } ; \epsilon ) \end{document} ]]></tex-math></inline-formula> in equation (5) and equating the terms with same powers of <inline-formula><tex-math id="math-44"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon , \end{document} ]]></tex-math></inline-formula> we get the following equations as,</p><disp-formula id="equation-9"><tex-math id="math-45"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array}{r l r l} \epsilon^ {0}: & D _ {0} ^ {2} q _ {0} + \Omega_ {0} ^ {2} q _ {0} & = & 0, \\ \epsilon^ {1}: & D _ {0} ^ {2} q _ {1} + \Omega_ {0} ^ {2} q _ {1} & = & - 2 D _ {1} D _ {0} q _ {0} - 2 \mu D _ {0} q _ {0} - \mathrm{I} q _ {0} ^ {3} \\ & & &  \end{array}\tag{9} \end{document} ]]></tex-math></disp-formula><disp-formula id="equation-10"><tex-math id="math-46"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle + (f _ {1} + 2 g _ {1} \cos \Omega_ {m} t) \sin \Omega t - k\tag{10} \end{document} ]]></tex-math></disp-formula><p>The general solution of equation <xref ref-type="disp-formula" rid="equation-9">(9)</xref> may be written as,</p><disp-formula id="equation-11"><tex-math id="math-47"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle q _ {0} (\mathrm{T} _ {0}, \mathrm{T} _ {1}) = A (\mathrm{T} _ {1}) e ^ {i \Omega_ {0} \mathrm{T} _ {0}} + A ^ {*} (\mathrm{T} _ {1}) e ^ {- i \Omega_ {0} \mathrm{T} _ {0}},\tag{11} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-48"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle A ( \mathrm { T } _ { 1 } ) \end{document} ]]></tex-math></inline-formula> and its complex conjugate <inline-formula><tex-math id="math-49"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle A ^ { * } ( \mathrm { { T } _ { 1 } ) } \end{document} ]]></tex-math></inline-formula> are functions of <inline-formula><tex-math id="math-50"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm { T _ { 1 } } \end{document} ]]></tex-math></inline-formula> . It may be noted that <inline-formula><tex-math id="math-51"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle A ( \mathrm { T } _ { 1 } ) \end{document} ]]></tex-math></inline-formula> ) and its conjugate need to be determined. Following the method described in Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>, the solution for <inline-formula><tex-math id="math-52"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle A ( \mathrm { T } _ { 1 } ) \end{document} ]]></tex-math></inline-formula> can be represented in polar form as</p><disp-formula id="equation-12"><tex-math id="math-53"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle A \left(\mathrm{T} _ {1}\right) = \frac {1}{2} a \left(\mathrm{T} _ {1}\right) \exp \left\{i \phi \left(\mathrm{T} _ {1}\right) \right\} \quad \text { and } \quad A ^ {*} \left(\mathrm{T} _ {1}\right) = \frac {1}{2} a \left(\mathrm{T} _ {1}\right) \exp \left\{- i \phi \left(\mathrm{T} _ {1}\right) \right\},\tag{12} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-54"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle a ( T _ { 1 } ) \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-55"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \phi ( T _ { 1 } ) \end{document} ]]></tex-math></inline-formula> refers to the amplitude and phase of the response.</p><p>As a result of substitution for <inline-formula><tex-math id="math-56"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle q _ { 0 } ( \mathrm { T } _ { 0 } , \mathrm { T } _ { 1 } ) \end{document} ]]></tex-math></inline-formula> , from equation (11), in equation (10), we get</p><disp-formula id="equation-13"><tex-math id="math-57"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array}{r c l} D _ {0} ^ {2} q _ {1} + \Omega_ {0} ^ {2} q _ {1} & = & - \left\{2 i \Omega_ {0} A ^ {\prime} + 2 i \mu \Omega_ {0} A + 3 A ^ {2} A ^ {*} I \right\} e ^ {i \Omega_ {0} \mathrm{T} _ {0}} - \mathrm{I} _ {2} A ^ {3} e ^ {3 i \Omega_ {0} \mathrm{T} _ {0}} \\ & - & \frac {i}{2} \left[ f _ {1} e ^ {i \Omega t} + g _ {1} \left\{e ^ {i (\Omega + \Omega_ {m}) t} + e ^ {i (\Omega - \Omega_ {m}) t} \right\} \right] - k + \mathrm{cc}, \end{array}\tag{13} \end{document} ]]></tex-math></disp-formula><p>where <sup>′</sup> denotes the derivative with respect to <inline-formula><tex-math id="math-58"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm { T _ { 1 } } \end{document} ]]></tex-math></inline-formula> and cc represents complex conjugate terms. Considering the setting where the main external forcing frequency is close to the system’s natural frequency, <inline-formula><tex-math id="math-59"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { 0 } \end{document} ]]></tex-math></inline-formula> , we may write Ω in terms of detuning parameter σ as,</p><disp-formula id="equation-14"><tex-math id="math-60"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega \equiv \Omega_ {0} + \epsilon \sigma .\tag{14} \end{document} ]]></tex-math></disp-formula><p>Depending on the values of excitation and modulating frequencies, we consider the following diferent scenarios, <inline-formula><tex-math id="math-61"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm{(i)} \Omega_ {m} < < \Omega , \quad \mathrm{(ii)} \Omega_ {m} = \Omega . \end{document} ]]></tex-math></inline-formula> In general, as in the case of communication engineering (Kennedy, Davis and Prasanna <xref ref-type="bibr" rid="BIBR-21">[21]</xref>), the modulating frequency <inline-formula><tex-math id="math-62"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { m } \end{document} ]]></tex-math></inline-formula> is much less than that of the excitation or carrier frequency, Ω. Therefore, using definitions viz., equations (12) and (14), equation (13) becomes</p><disp-formula id="equation-15"><tex-math id="math-63"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{align*}D_0^2 q_1 + \Omega_0^2 q_1 = {} & -\left\{ i\Omega_0(a' + ia\phi') + i\Omega_0 \mu a + \dfrac{3}{8}a^3 I + \dfrac{i}{2}(f_1 + 2g_1)e^{i(\sigma T_1 - \phi)} \right\} \times \nonumber \\& \times \ e^{i(\Omega_0 T_0 + \phi)} - \dfrac{1}{8}a^3 e^{3i(\Omega_0 T_0 + \phi)} - k + cc.\end{align*}\tag{15} \end{document} ]]></tex-math></disp-formula><p>Putting <inline-formula><tex-math id="math-64"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma \mathrm { T } _ { 1 } - \phi = \gamma \end{document} ]]></tex-math></inline-formula> and then equating the secular term to zero, we get the following equations for the amplitude and phase response of the present Dufing type system as,</p><disp-formula id="equation-16"><tex-math id="math-65"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega_ {0} a ^ {\prime} = - \Omega_ {0} \mu a - \frac {f _ {1} + 2 g _ {1}}{2} \cos \gamma ,\tag{16} \end{document} ]]></tex-math></disp-formula><disp-formula id="equation-17"><tex-math id="math-66"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega_ {0} a \gamma^ {\prime} = \Omega_ {0} \sigma a - \frac {3}{8} \mathrm{I} a ^ {3} + \frac {f _ {1} + 2 g _ {1}}{2} \sin \gamma .\tag{17} \end{document} ]]></tex-math></disp-formula><p>The foregoing expression for the amplitude and phase response results in the relation for the detuning parameter <inline-formula><tex-math id="math-67"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma , \end{document} ]]></tex-math></inline-formula> in the steady state as,</p><disp-formula id="equation-18"><tex-math id="math-68"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma = \frac {3 \mathrm{I}}{8 \Omega_ {0}} a ^ {2} \pm \left[ \frac {(f _ {1} + 2 g _ {1}) ^ {2}}{4 \Omega_ {0} ^ {2} a ^ {2}} - \mu^ {2} \right] ^ {1 / 2}.\tag{18} \end{document} ]]></tex-math></disp-formula><p>and hence the excitation frequency Ω near the resonant frequency, <inline-formula><tex-math id="math-69"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { 0 } \end{document} ]]></tex-math></inline-formula> , would be</p><disp-formula id="equation-19"><tex-math id="math-70"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega = \left(\Omega_ {0} + \epsilon \frac {3 \mathrm{I}}{8 \Omega_ {0}} a ^ {2}\right) \pm \epsilon \left[ \frac {(f _ {1} + 2 g _ {1}) ^ {2}}{4 \Omega_ {0} ^ {2} a ^ {2}} - \mu^ {2} \right] ^ {1 / 2},\tag{19} \end{document} ]]></tex-math></disp-formula><p>where the term <inline-formula><tex-math id="math-71"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { \left( \Omega _ { 0 } + \epsilon \ \frac { 3 I } { 8 \Omega _ { 0 } } a ^ { 2 } \right) } \end{array} \end{document} ]]></tex-math></inline-formula> defines the back-bone curve, i.e., frequency-amplitude relation of the undamped free oscillation of system.</p><p>From equation (16), the maximum value, that the amplitude of the oscillation can achieve, is given by</p><disp-formula id="equation-20"><tex-math id="math-72"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle a _ {m a x} = \frac {f _ {1} + 2 g _ {1}}{2 \Omega_ {0} \mu}\tag{20} \end{document} ]]></tex-math></disp-formula><p>The equation for amplitude response, in this case, is given by</p><disp-formula id="equation-21"><tex-math id="math-73"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \frac {a}{| f _ {1} + 2 g _ {1} |} = \frac {1}{2 \sqrt {\Omega_ {0} ^ {2} \mu^ {2} + (\Omega_ {0} \sigma - \frac {3}{8} I a ^ {2}) ^ {2}}}.\tag{21} \end{document} ]]></tex-math></disp-formula><p>Therefore, for the case (i), <inline-formula><tex-math id="math-74"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . , \ \Omega _ { m } \ < < \ \Omega . \end{document} ]]></tex-math></inline-formula> , the AME significantly afects the amplitude and phase response of the Dufing type system with weak damping, weak nonlinearity and weak AME forcing term. Fig. <xref ref-type="fig" rid="figure-1">2.1</xref> and Fig. <xref ref-type="fig" rid="figure-2">2.2</xref> show the pattern of variation of amplitude, a, with detuning parameter, σ, for specific values of modulation amplitude,and for diferent values of damping coeficient, <inline-formula><tex-math id="math-75"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mu . \end{document} ]]></tex-math></inline-formula></p><p>Direct simulation of equations <xref ref-type="disp-formula" rid="equation-16">(16)</xref> and <xref ref-type="disp-formula" rid="equation-17">(17)</xref> result in exhibiting the possibilities of coexistence of three equilibrium points, of which two are stable and one unstable saddle point (Fig. <xref ref-type="fig" rid="figure-3">2.3</xref>). It may be further noted that for case <inline-formula><tex-math id="math-76"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle ( i i ) \ i . e . , \ \Omega _ { m } = \Omega \end{document} ]]></tex-math></inline-formula> 2 the right hand side of the amplitude and phase responses, <inline-formula><tex-math id="math-77"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . , \end{document} ]]></tex-math></inline-formula> equations <xref ref-type="disp-formula" rid="equation-16">(16)</xref> and <xref ref-type="disp-formula" rid="equation-17">(17)</xref>, remain independent of the amplitude modulation term, <inline-formula><tex-math id="math-78"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle g _ { 1 } \end{document} ]]></tex-math></inline-formula>.</p><p>, <inline-formula><tex-math id="math-79"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle g_1 \end{document} ]]></tex-math></inline-formula></p><fig id="figure-1"><label>Figure 2.1.</label><caption><p>Frequency  Response  curve  for  different  values  ofmodulation parameter</p></caption><graphic xlink:href="https://jims-a.org/index.php/jimsa/article/download/1709/574/14269" mime-subtype="jpeg" mimetype="image"><alt-text>Figure 2.1.</alt-text></graphic></fig></sec><sec id="sec-4"><title>2.2. Response of the strongly nonlinear AME excited Dufingtype system using Modified Multi Time Scale Perturbation Method.</title><p>In this section, we consider the strongly damped and nonlinear AME excited Dufing type system. In such a case, we need to incorporate modifications in the foregoing analysis. Therefore, with the following details, the present analysis in this section is termed as modified multi time scale perturbation method (hereafter MMTPM). Following Nayfeh and Mook <xref ref-type="bibr" rid="BIBR-7">[7]</xref>, we need to replace the expansion parameter, ϵ, in the MTPM by a new parameter, <inline-formula><tex-math id="math-80"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha = \alpha ( \epsilon ) \end{document} ]]></tex-math></inline-formula> . Such a change is facilitated by first redefining the squared frequency, <inline-formula><tex-math id="math-81"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega ^ { 2 } \end{document} ]]></tex-math></inline-formula> , of the forced Dufing system in terms of detuning parameter, <inline-formula><tex-math id="math-82"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma _ { : } \end{document} ]]></tex-math></inline-formula> , and the parameter, α, as</p><disp-formula id="equation-22"><tex-math id="math-83"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega^ {2} = p \left(\Omega_ {0} ^ {2} + \frac {3}{4} \epsilon a _ {0} ^ {2}\right) [ 1 + \alpha \sigma ],\tag{22} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-84"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle p \end{document} ]]></tex-math></inline-formula> is a constant while <inline-formula><tex-math id="math-85"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle a _ { 0 } \end{document} ]]></tex-math></inline-formula> refers to the amplitude of the fundamental harmonic. Subsequently the parameter α may be defined as,</p><disp-formula id="equation-23"><tex-math id="math-86"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha = \frac {\epsilon a _ {0} ^ {2}}{4 \left(\Omega_ {0} ^ {2} + \frac {3}{4} \epsilon a _ {0} ^ {2}\right)}\tag{23} \end{document} ]]></tex-math></disp-formula><fig id="figure-2"><label>Figure 2.2.</label><caption><p>Frequency  Response  curve  for  different  values  ofdamping parameter, (μ).</p></caption><graphic xlink:href="https://jims-a.org/index.php/jimsa/article/download/1709/574/14270" mime-subtype="jpeg" mimetype="image"><alt-text>Figure 2.2.</alt-text></graphic></fig><fig id="figure-3"><label>Figure 2.3.</label><caption><p>Three  coexisting  equilibrium  solution  of  eqs.(2.14-2.15) with f1= 0.25, μ = 0.10,  Ω = 1.2,ε = 0.2 and I = 5.0</p></caption><graphic xlink:href="https://jims-a.org/index.php/jimsa/article/download/1709/574/14271" mime-subtype="jpeg" mimetype="image"><alt-text>Figure 2.3.</alt-text></graphic></fig><p>As a result, for arbitrarily large values of the term <inline-formula><tex-math id="math-87"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon a _ { 0 } ^ { 2 } , \end{document} ]]></tex-math></inline-formula> , note that the parameter, α get restricted to the value of <inline-formula><tex-math id="math-88"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \leq \frac { 1 } { 3 } \end{document} ]]></tex-math></inline-formula> . The relation between the parameter, ϵ and α may therefore be written as,</p><disp-formula id="equation-24"><tex-math id="math-89"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon = \frac {4 \alpha}{a _ {0} ^ {2} (1 - 3 \alpha)} \Omega_ {0} ^ {2}.\tag{24} \end{document} ]]></tex-math></disp-formula><p>Therefore, using equations <xref ref-type="disp-formula" rid="equation-23">(23)</xref> and <xref ref-type="disp-formula" rid="equation-24">(24)</xref> into equation <xref ref-type="disp-formula" rid="equation-22">(22)</xref>, it is readily observed that</p><disp-formula id="equation-25"><tex-math id="math-90"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega \simeq \sqrt {p} \Omega_ {0} + \alpha \sigma_ {M},\tag{25} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-91"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { \sigma _ { M } = \sqrt { p } \frac { \Omega _ { 0 } ( 3 + \sigma ) } { 2 } } \end{array} \end{document} ]]></tex-math></inline-formula> and may be termed as modified detuning parameter.</p><p>Having introduced the parameter, α, and <inline-formula><tex-math id="math-92"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega ^ { 2 } \end{document} ]]></tex-math></inline-formula> , we may recast, equation <xref ref-type="disp-formula" rid="equation-5">(5)</xref>, using the Lindstedt-Poinc´are transformation, as <inline-formula><tex-math id="math-93"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm { T } = \Omega t \end{document} ]]></tex-math></inline-formula> (Mickens <xref ref-type="bibr" rid="BIBR-13">[13]</xref>), to get</p><disp-formula id="equation-26"><tex-math id="math-94"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega^ {2} q ^ {\prime \prime} + 2 \epsilon \mu \Omega q ^ {\prime} + \Omega_ {0} ^ {2} q + \epsilon \mathrm{I} q ^ {3} = \epsilon \left[ \left\{f _ {1} + 2 g _ {1} \cos \frac {\Omega_ {m}}{\Omega} \mathrm{T} \right\} \sin \mathrm{T} - k \right].\tag{26} \end{document} ]]></tex-math></disp-formula><p>Here, <sup>′</sup> represents derivative with respect to T. Further substitution of ϵ and <inline-formula><tex-math id="math-95"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega ^ { 2 } \end{document} ]]></tex-math></inline-formula> from equations <xref ref-type="disp-formula" rid="equation-22">(22)</xref> and <xref ref-type="disp-formula" rid="equation-24">(24)</xref>, last equation results in</p><disp-formula id="equation-27"><tex-math id="math-96"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array}{r c l} (1 + \alpha \sigma) q ^ {\prime \prime} + \frac {(1 - 3 \alpha)}{p} q & + & \frac {4 \alpha}{a _ {0} ^ {2} p} 2 \mu \Omega q ^ {\prime} + \frac {4 \alpha}{a _ {0} ^ {2} p} \mathrm{I} q ^ {3} \\ & = & \frac {4 \alpha}{a _ {0} ^ {2} p} \left[ \left\{f _ {1} + 2 g _ {1} \cos \frac {\Omega_ {m}}{\Omega} \mathrm{T} \right\} \sin \mathrm{T} - k \right]. \end{array}\tag{27} \end{document} ]]></tex-math></disp-formula><p>Non-dimensionalizing q by defining <inline-formula><tex-math id="math-97"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { u = \frac { q } { a _ { 0 } } } \end{array} \end{document} ]]></tex-math></inline-formula> , equation <xref ref-type="disp-formula" rid="equation-27">(27)</xref> takes the following form</p><disp-formula id="equation-28"><tex-math id="math-98"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle (1 + \alpha \sigma) u ^ {\prime \prime} + 2 \alpha \eta u ^ {\prime} + \frac {(1 - 3 \alpha)}{p} u + 4 \frac {\alpha}{p} \mathrm{I} u ^ {3} = \alpha \left[ \left\{F + 2 G \cos \frac {\Omega_ {m}}{\Omega} \mathrm{T} \right\} \sin \mathrm{T} - K \right],\tag{28} \end{document} ]]></tex-math></disp-formula><p>where various factors have been redefined as follows</p><disp-formula id="equation-29"><tex-math id="math-99"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \eta = \frac {4 \Omega}{a _ {0} ^ {2} p} \mu , F = \frac {4 f _ {1}}{a _ {0} ^ {3} p}, G = \frac {4 g _ {1}}{a _ {0} ^ {3} p} \mathrm{and} K = \frac {4}{a _ {0} ^ {3} p} k.\tag{29} \end{document} ]]></tex-math></disp-formula><p>With <inline-formula><tex-math id="math-100"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { m } < < \Omega \end{document} ]]></tex-math></inline-formula> , equation <xref ref-type="disp-formula" rid="equation-28">(28)</xref> may be rewritten as,</p><disp-formula id="equation-30"><tex-math id="math-101"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle (1 + \alpha \sigma) u ^ {\prime \prime} + 2 \alpha \eta u ^ {\prime} + \frac {(1 - 3 \alpha)}{p} u + 4 \frac {\alpha I}{p} u ^ {3} = \alpha \{F + 2 G \} \sin T - \alpha K.\tag{30} \end{document} ]]></tex-math></disp-formula><p>The improved multiple scales method, <inline-formula><tex-math id="math-102"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle i . e . \end{document} ]]></tex-math></inline-formula> , MMTPM, with the new expansion parameter <inline-formula><tex-math id="math-103"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha , \end{document} ]]></tex-math></inline-formula> time scales are defined as follows</p><disp-formula id="equation-31"><tex-math id="math-104"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm{T} _ {n} = \alpha^ {n} \mathrm{T}, \quad \Longrightarrow \quad \frac {d}{d \mathrm{T}} = D _ {0} + \alpha D _ {1} + \dots \text { and } \frac {d ^ {2}}{d \mathrm{T} ^ {2}} = D _ {0} ^ {2} + 2 \alpha D _ {1} D _ {0} + \dots ,\tag{31} \end{document} ]]></tex-math></disp-formula><p>and is used again to analyze primary resonances for system <xref ref-type="disp-formula" rid="equation-30">(30)</xref>. Let the solution of equation <xref ref-type="disp-formula" rid="equation-30">(30)</xref>, as earlier, be assumed as,</p><disp-formula id="equation-32"><tex-math id="math-105"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle u (\alpha ; \mathrm{T}) = u _ {0} (\mathrm{T} _ {0}, \mathrm{T} _ {1}, \dots) + \alpha u _ {1} (\mathrm{T} _ {0}, \mathrm{T} _ {1} \dots) + \dots .\tag{32} \end{document} ]]></tex-math></disp-formula><p>Using equations <xref ref-type="disp-formula" rid="equation-31">(31)</xref> and <xref ref-type="disp-formula" rid="equation-32">(32)</xref>, up to first order in <inline-formula><tex-math id="math-106"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha , \end{document} ]]></tex-math></inline-formula> equation <xref ref-type="disp-formula" rid="equation-30">(30)</xref> becomes</p><disp-formula id="equation-33"><tex-math id="math-107"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{align*}& (1 + \alpha\sigma)D_0^2 u_0 + \alpha D_0^2 u_1 + 2\alpha D_1 D_0 u_0 + 2\alpha\eta D_0 u_0 + \frac{1-3\alpha}{p}u_0 + \frac{1}{p}\alpha u_1 \\& + \frac{4}{p}\alpha\mathrm{I}u_0^3 = \alpha\{F + 2G\}\sin T - \alpha K.\end{align*}\tag{33} \end{document} ]]></tex-math></disp-formula><p>Further equating coeficient of powers of <inline-formula><tex-math id="math-108"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha , \end{document} ]]></tex-math></inline-formula> equation <xref ref-type="disp-formula" rid="equation-33">(33)</xref> results in following two equations</p><disp-formula id="equation-34"><tex-math id="math-109"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \alpha^ {0}: \quad D _ {0} ^ {2} u _ {0} + \frac {1}{p} u _ {0} = 0,\tag{34} \end{document} ]]></tex-math></disp-formula><disp-formula id="equation-35"><tex-math id="math-110"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{align*}\alpha^1: \quad & D_0^2 u_1 + \frac{1}{p}u_1 = -\sigma D_0^2 u_0 - 2D_1 D_0 u_0 - 2\eta D_0 u_0 + \frac{3}{p}u_0 - \frac{4}{p}\mathrm{I}u_0^3 \\& + (F + 2G)\sin T - K\end{align*}\tag{35} \end{document} ]]></tex-math></disp-formula><p>Based on equations <xref ref-type="disp-formula" rid="equation-11">(11)</xref> and <xref ref-type="disp-formula" rid="equation-12">(12)</xref>, it readily follows that</p><disp-formula id="equation-36"><tex-math id="math-111"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle u _ {0} \left(\mathrm{T} _ {0}, \mathrm{T} _ {1}\right) = \frac {a}{2} \exp \left\{i \left(\frac {\mathrm{T} _ {0}}{\sqrt {p}} + \phi\right) \right\} + c c,\tag{36} \end{document} ]]></tex-math></disp-formula><p>where a and <inline-formula><tex-math id="math-112"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \phi \end{document} ]]></tex-math></inline-formula> have the same meaning as in section (2.1).</p><p>Substitution of equation <xref ref-type="disp-formula" rid="equation-36">(36)</xref> into <xref ref-type="disp-formula" rid="equation-35">(35)</xref> results in</p><disp-formula id="equation-37"><tex-math id="math-113"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array}{r c l}D_0^2 u_1 + \frac{1}{p}u_1 & = & \left[ \frac{1}{2p}\sigma a - i\frac{a'}{\sqrt{p}} + a\frac{\phi'}{\sqrt{p}} - i\eta\frac{a}{\sqrt{p}} + \frac{3}{2p}a(1 - Ia^2) \right] e^{\left\{i\left(\frac{T_0}{\sqrt{p}} + \phi\right)\right\}} \\& - & \frac{I}{2p}a^3 e^{3i\left(\frac{T_0}{\sqrt{p}} + \phi\right)} - K - \frac{i}{2}(F + 2G)e^{iT_0} + cc.\end{array}\tag{37} \end{document} ]]></tex-math></disp-formula><p>It may be noted that oscillator in equation (33) corresponds to the normalized natural frequency <inline-formula><tex-math id="math-114"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { \omega = \frac { 1 } { \sqrt { p } } } \end{array} \end{document} ]]></tex-math></inline-formula> whereas the external frequency Ω is normalized to 1. Therefore, for primary resonance to occur, <inline-formula><tex-math id="math-115"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle p = 1 \end{document} ]]></tex-math></inline-formula> . In that event, the AME excitation term contributes to the secular term in the solution to equation <xref ref-type="disp-formula" rid="equation-37">(37).</xref> Therefore, on eliminating the resulting secular terms, we obtain the following set of equations for the amplitude and phase response as,</p><disp-formula id="equation-38"><tex-math id="math-116"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle {a ^ {\prime}} = {- \eta a - \frac {(F + 2 G)}{2} \cos \phi ,}\tag{38} \end{document} ]]></tex-math></disp-formula><disp-formula id="equation-39"><tex-math id="math-117"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle {a \phi^ {\prime}} = {- \frac {\sigma a}{2} - \frac {3}{2} a (1 - I a ^ {2}) + \frac {(F + 2 G)}{2} \sin \phi .}\tag{39} \end{document} ]]></tex-math></disp-formula><p>In the steady state, for <inline-formula><tex-math id="math-118"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I = 1 \end{document} ]]></tex-math></inline-formula> , the amplitude <inline-formula><tex-math id="math-119"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle a 1 \end{document} ]]></tex-math></inline-formula> . Therefore detuning frequency, σ, at the steady state may be written as,</p><disp-formula id="equation-40"><tex-math id="math-120"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \sigma = - Z _ {1} \pm \sqrt {Z _ {1} ^ {2} + Z _ {2}},\tag{40} \end{document} ]]></tex-math></disp-formula><p>where <inline-formula><tex-math id="math-121"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { Z _ { 1 } = - \frac { 3 2 \mu ^ { 2 } \alpha } { I ^ { 2 } a _ { 0 } ^ { 4 } ( 1 - 3 \alpha ) } } \end{array} \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-122"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { Z _ { 2 } = \frac { 6 4 } { I ^ { 2 } a _ { 0 } ^ { 4 } } \Bigg \lceil \bigg ( \frac { F + 2 G } { a _ { 0 } } \bigg ) ^ { 2 } - \frac { \mu ^ { 2 } \Omega _ { 0 } ^ { 2 } } { 1 - 3 \alpha } \Bigg \rceil } \end{array} \end{document} ]]></tex-math></inline-formula> . The efect of AME excited steady state amplitude response curve, for <inline-formula><tex-math id="math-123"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Omega _ { m } < \dot { < } \Omega \end{document} ]]></tex-math></inline-formula> , is shown in Fig. <xref ref-type="fig" rid="figure-4">2.4</xref> for diferent values of the parameter, ϵ. It is to be noted that the maximum amplitude, <inline-formula><tex-math id="math-124"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \begin{array} { r } { a _ { m a x } = \left( \frac { F + 2 G } { \mu \Omega _ { 0 } } \right) \sqrt { 1 - 3 \alpha } } \end{array} \end{document} ]]></tex-math></inline-formula> and therefore tends to reduce with increase in ϵ while retaining other parameter values. The MMTPM, therefore, enables us to obtain the amplitudefrequency response curve even for larger values of the parameter, ϵ.</p><fig id="figure-4"><label>Figure 2.4.</label><caption><p>Amplitude-frequency  Response  curve  for  varying εin AME excited Duffing type oscillator.</p></caption><graphic xlink:href="https://jims-a.org/index.php/jimsa/article/download/1709/574/14272" mime-subtype="jpeg" mimetype="image"><alt-text>Figure 2.4.</alt-text></graphic></fig></sec></sec><sec id="sec-5"><title>3. MAIN RESULTS</title><p>In this paper, the problem of a DufingHelmholtz oscillator excited by an amplitude modulated signal is considered. Using Cardano’s transformation, the problem is shown to get reduced to a Dufing -type system excited by an amplitude modulated (AME) signal and a constant bias signal that depends on the parameters of the original system. Assuming the excitation amplitudes <inline-formula><tex-math id="math-125"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \left( f _ { 1 } \right) \end{document} ]]></tex-math></inline-formula> , modulation <inline-formula><tex-math id="math-126"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mathrm { a m p l i t u d e } ( g _ { 1 } ) \end{document} ]]></tex-math></inline-formula> , damping <inline-formula><tex-math id="math-127"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle ( \mu ) \end{document} ]]></tex-math></inline-formula> and nonlinearity parameter, <inline-formula><tex-math id="math-128"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle I , \end{document} ]]></tex-math></inline-formula> to be a perturbation on the system, a multi time scale perturbation method (MTPM) involving an expansion parameter, <inline-formula><tex-math id="math-129"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon , \end{document} ]]></tex-math></inline-formula> has been used to understand the dynamical complexities involved in getting the amplitudefrequency relationship, exhibiting bi-stability on varying the modulation parameter, <inline-formula><tex-math id="math-130"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle g _ { 1 } \end{document} ]]></tex-math></inline-formula> , and the damping parameter, <inline-formula><tex-math id="math-131"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \mu , \end{document} ]]></tex-math></inline-formula> of the Dufing-type system (Figs.<xref ref-type="fig" rid="figure-1">2.1</xref>-<xref ref-type="fig" rid="figure-2">2.2</xref>) near primary-resonance. Phase plane trajectories exhibiting the stable and unstable manifolds for specific values of the parameters involved in the system is further illustrated in Fig.<xref ref-type="fig" rid="figure-3">2.3</xref>.</p><p>A modified perturbation scheme (MMTPM) extending the MTPM scheme is further developed, incorporating the Lindstedt-Poincare transformation and a transformation <inline-formula><tex-math id="math-132"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon \alpha \end{document} ]]></tex-math></inline-formula> , so as to obtain the response of the AME excited Dufing -type system even for very high values of the parameter, ϵ i.e, strongly nonlinear system. Simulation results showing the amplitude-frequency response around the back bone curve for <inline-formula><tex-math id="math-133"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon = 0 . 5 \end{document} ]]></tex-math></inline-formula> and <inline-formula><tex-math id="math-134"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon = 1 . 0 \end{document} ]]></tex-math></inline-formula> , as obtained in Fig.<xref ref-type="fig" rid="figure-4">2.4</xref> further reveal the bi-stable behavior of the system. For the parameter of the Dufing-type system as given in Fig.<xref ref-type="fig" rid="figure-4">2.4</xref>, the peak amplitude, <inline-formula><tex-math id="math-135"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle a _ { m a x } \end{document} ]]></tex-math></inline-formula> for <inline-formula><tex-math id="math-136"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon = 0 . 5 \end{document} ]]></tex-math></inline-formula> is observed to be larger than that when <inline-formula><tex-math id="math-137"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \epsilon = 1 . 0 . \end{document} ]]></tex-math></inline-formula></p><p><bold>Appendix A.</bold></p><p>The linear stability analysis of the amplitude and phase response for theDuffing-type system can be analyzed by considering equations <xref ref-type="disp-formula" rid="equation-16">(16)</xref>-<xref ref-type="disp-formula" rid="equation-17">(17)</xref> and writingits Jacobian matrix as,</p><disp-formula id="equation-41"><tex-math id="math-138"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle J = \begin{vmatrix} -\xi & \theta\sin\gamma \\ \dfrac{\left(\sigma - \frac{9}{8}Ia^2\right)}{a} & \theta\cos\gamma \end{vmatrix} = \begin{vmatrix} -\xi & -a\left[\sigma - \dfrac{3Ia^2}{8\Omega_0}\right] \\ \dfrac{\left(\sigma - \frac{9Ia^2}{8}\right)}{a} & -\xi \end{vmatrix},\tag{A.1} \end{document} ]]></tex-math></disp-formula><p>Where <inline-formula><tex-math id="math-139"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \theta = \dfrac{f_1 + 2g_1}{2\Omega_0}. \end{document} ]]></tex-math></inline-formula></p><p>The characteristic roots, λ1,2, may therefore be written as,</p><disp-formula id="equation-42"><tex-math id="math-140"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \lambda_{1,2} = -\xi \pm \sqrt{\left(\sigma - \dfrac{3Ia^2}{8\Omega_0}\right)\left(\dfrac{9Ia^2}{8\Omega_0} - \sigma\right)}\tag{A.2} \end{document} ]]></tex-math></disp-formula><p>Alternatively, it is observed that, the determinant, ∆, and the trace of J , are given by,</p><disp-formula id="equation-43"><tex-math id="math-141"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Delta = \det(J) = \xi^2 + \left(\sigma - \dfrac{3Ia^2}{8\Omega_0}\right)\left(\dfrac{9Ia^2}{8\Omega_0} - \sigma\right); \quad \text{Tr}(J) = -2\xi.\tag{A.3} \end{document} ]]></tex-math></disp-formula><fig id="figure-5"><label>Figure 3.5.</label><caption><p>Frequency response diagram in case of AME excitedDuffing-type oscillator based on MTPM</p></caption><graphic xlink:href="https://jims-a.org/index.php/jimsa/article/download/1709/574/14273" mime-subtype="png" mimetype="image"><alt-text>Figure 3.5.</alt-text></graphic></fig><disp-formula id="equation-44"><tex-math id="math-142"><![CDATA[ \documentclass{article} \usepackage{amsmath} \begin{document} \displaystyle \Delta = \xi^2 + \left(\sigma - \dfrac{3}{8}Ia^2\right)\left(\dfrac{9}{8}Ia^2 - \sigma\right) = 0\tag{A.4} \end{document} ]]></tex-math></disp-formula><p>It is to be noted that, sum of the eigenvalues, i.e., Tr(J ), is negative. There-fore, for the stability of the fixed point of the amplitude and phase response, boththe  eigenvalues viz., λ1,2should have negative real part. However, if one of theeigenvalue say λ1is having negative real part, then the fixed point of the systemwould be saddle only if the real part of the other eigenvalue (λ2), is positive. Incase, one of the eigenvalue, say λ2, is zero, then the system undergoes a bifurcation,i.e., saddle node/ pitch-fork bifurcation and the following condition holds,</p><p>A typical frequency-response curve is shown in Fig.<xref ref-type="fig" rid="figure-5">3.5</xref> where the point P2andP3refers to the jump-up and jump-down points respectively.The curve between thepoint P2and P3corresponds  to the unstable domain, whereas the curve joiningthe points P1, X1and P3along with the curve joining P2, X3and P4refers to thestable region (Kalḿar-Nagy and Balachandran <xref ref-type="bibr" rid="BIBR-11">[11]</xref>).</p></sec></body><back><sec sec-type="data-availability"><title>Data Availability Statement.</title><p>No data was used for the research described in the article.</p></sec><sec sec-type="author-contributions"><title>Author Contributions.</title><p>Chaudhary Anunay Kumar: Conceptualization, formal analysis, writingoriginal draft, editing, methodology. Das Saureesh: Conceptualization, final draft, editing, methodology, software. Narang Pankaj: Conceptualization, final draft, editing, methodology, software. 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