Adaptive Backstepping Control for Hypersonic Vehicles with Actuator Amplitude and Rate Saturation

• 作 者: XIANG Kai DU Yanli ZHANG Peng
• 机 构: CollegeofAstronautics
• 出 处: 南京航空航天大学学报:英文版
• 发表日期: 2019年2期
• 关键词: HYPERSONIC vehicle AMPLITUDE and RATE SATURATION adaptive BACKSTEPPING aerodynam
• 基金项目: the National Natural Science Foundation of China(No.61304099),the Foundation of Graduate Innovation Center in NUAA(No.kfjj20171505),the Postgraduate Research&Practice Innovation Program of Jiangsu

This paper presents a constrained control strategy for the hypersonic vehicle with actuator amplitude,rate constraints and aerodynamic uncertainties.First,a vehicle-actuator control model is derived in consideration of actuator dynamics properties explici