Title :
Nonlinear pneumatic/ thrust vectoring composite control Design for one nearspace hypersonic aircraft
Author :
Jie, Chen ; Yong, Liang ; Chao, Song
Author_Institution :
Naval Aeronaut. & Astronaut. Univ., Yantai, China
Abstract :
One nearspace hypersonic aircraft model based on pneumatic/thrust vectoring composite control was built, compound controler optimization scheme was adopted to cooperate pneumatic/thrust vectoring compound controler equivalent dynamic characteristic to reference model during dynamic assign.The simulation result shows the arithmetic availability.
Keywords :
aerospace propulsion; aircraft control; control system synthesis; nonlinear control systems; optimisation; pneumatic control equipment; arithmetic availability; compound controller equivalent dynamic characteristics; compound controller optimization scheme; nearspace hypersonic aircraft model; nonlinear pneumatic-thrust vectoring composite control design; reference model; Adaptation models; Aerospace control; Aircraft; Atmospheric modeling; Educational institutions; Electronic mail; Military aircraft; A six degree-of-free nonlinear model; Adaptive backstepping control; Composite control; Hypersonic aircraft;
Conference_Titel :
Control and Decision Conference (CCDC), 2012 24th Chinese
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4577-2073-4
DOI :
10.1109/CCDC.2012.6244454
