Aero-thermal heating constrained midcourse guidance using state-constrained model predictive static programming method

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    摘要 Thispaperproposesamultiple-constraints-guaranteedmidcourseguidancelawfortheinterceptionofthehypersonictargets.Intraditionalmidcourselawdesign,theconstraintsoftheaero-thermalheatingarerarelytakenintoconsideration.Theperformanceoftheinfrareddetectionsystemmaybedegradedandtheinstabilityoftheflightcontrolsystemmaybeinduced.Toaddressthisproblem,astate-constrainedmodelpredictivestaticprogrammingmethodisintroducedsuchthatbothterminalconstraints(positionandangle)andoptimalenergyconsumptioncanbeensured.Asaresult,asub-optimalmidcourseguidance,guaranteeingtheaforementionedmultiple-constraintstobeneverviolated,issynthesized.Simulationresultsdemonstratetheeffectivenessoftheproposedmethod.
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    出版日期 2018年06月16日(中国Betway体育网页登陆平台首次上网日期,不代表论文的发表时间)
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