简介：Aimingathandlingcomplicatedmaneuversorotherunpredictedemergenciesforhypersonicglidevehicletracking,threecoupleddynamicmodelsofstateestimationbasedontheprioriinformationbetweenguidancevariablesandaerodynamicsarepresented.Firstly,theaerodynamicaccelerationactingonthetargetisanalyzedtorevealtheessenceofthetarget’smotion.Thenthreecoupledstructuresformodelingaerodynamicparametersaredevelopedbydifferentideas:thespiralmodelwithaharmonicoscillator,thebankmodelwithtrigonometricfunctionsofthebankangleandtheguidemodelwiththechangingruleofguidancevariables.Meanwhile,thecomparisondiscussionisconcludedtoshowthenoveltyandadvantageofthesemodels.Finally,aperformanceassessmentindifferentsimulationcasesispresentedanddetailedanalysisisrevealed.Theresultsshowthattheproposedmodelsperformexcellentproperties.Moreover,theguidemodelproducesthebesttrackingperformanceandthebankmodelshowsthesecond;however,thespiralmodeldoesnotoutperformthemaneuveringreentryvehicle(MaRV)modelmarkedly.

简介：本文讲述了AVLGLIDE软件的分析与评价方法，并以某83a活塞的型线设计开发为例，介绍了基于GLIDE软件的活塞型线及其他动力性能参数的优化过程，并通过试验进行了验证。实验结果证明，GLIDE软件可有效的模拟活塞运动过程，进行活塞动力学的计算，对于活塞的设计及优化具有重要的意义。