Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle

被引：3
|
作者：
Ren, Zijun [1 ]
Fu, Wenxing [1 ]
Yan, Jie [1 ]
Xu, Bin [2 ,3 ]
机构：
[1] Northwestern Polytech Univ, Sch Astronaut, Xian, Peoples R China
[2] Northwestern Polytech Univ, Sch Automat, Xian 710129, Peoples R China
[3] Northwestern Polytech Univ Shenzhen, Res Inst, Shenzhen, Peoples R China
来源：
ADVANCES IN MECHANICAL ENGINEERING | 2017年 / 9卷 / 04期
基金：
中国国家自然科学基金;
关键词：
Control theory; adaptive control; system and control theory; aerodynamics; system modeling; ADAPTIVE NEURAL-CONTROL; BACKSTEPPING CONTROL; SYSTEMS; DESIGN;
D O I：
10.1177/1687814017703900
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
A discrete reconfigurable back-stepping controller is proposed to resolve the attitude command tracking problem of hypersonic flight vehicle in reentry mode. The hypersonic flight vehicle dynamic equations are transformed into discrete form based on Euler numerical integration method. Discrete control command is designed via discrete back-stepping. Control allocation strategy is introduced to deal with the resource distributing problem of reaction control system and aero-surfaces. In computer simulation environment, the vehicle tracks command signals precisely and quickly.
引用
收藏
页码：1 / 10
页数：10
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