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  • 简介:Thispaperproposesamultiple-constraints-guaranteedmidcourseguidancelawfortheinterceptionofthehypersonictargets.Intraditionalmidcourselawdesign,theconstraintsoftheaero-thermalheatingarerarelytakenintoconsideration.Theperformanceoftheinfrareddetectionsystemmaybedegradedandtheinstabilityoftheflightcontrolsystemmaybeinduced.Toaddressthisproblem,astate-constrainedmodelpredictivestaticprogrammingmethodisintroducedsuchthatbothterminalconstraints(positionandangle)andoptimalenergyconsumptioncanbeensured.Asaresult,asub-optimalmidcourseguidance,guaranteeingtheaforementionedmultiple-constraintstobeneverviolated,issynthesized.Simulationresultsdemonstratetheeffectivenessoftheproposedmethod.

  • 标签: MIDCOURSE guidance model PREDICTIVE CONTROL optimal
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