One nearspace hypersonic aircraft dynamic surface adative backstepping control design based on nonlinear neumatic/ thrust vectoring composite control

One nearspace hypersonic aircraft model based on pneumatic/ thrust vectoring composite control was built, compound controller optimization scheme was adopted to cooperate pneumatic/thrust vectoring compound controller equivalent dynamic characteristic to reference model during dynamic assign. In the...

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Bibliographische Detailangaben

Hauptverfasser:	Shaowu Dai, Jie Chen, Chao Song
Format:	Tagungsbericht
Sprache:	chi ; eng
Schlagworte:	a six degree-of-freedomnonlinear model Adaptation models Aerodynamics Aerospace control Aircraft Atmospheric modeling Backstepping composite control dynamic surface adative backstepping control Educational institutions hypersonic aircraft
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