Lateral-directional Attitude Under-actuated Control Strategy of Hypersonic Vehicle

被引:0
|
作者
Niu, Yike [1 ]
Sun, Chunzhen [1 ]
Huang, Yimin [1 ]
Wang, Xin [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Sch Automat, Nanjing, Jiangsu, Peoples R China
关键词
Hypersonic vehicle; Under-actuated; Cascade control;
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
Research on lateral-directional attitude under-actuated control of the hypersonic vehicle with only the aileron, a new lateral-directional control strategy based on the idea of cascade was proposed, that can realize the roll angle control and guarantee the stabilization of the sideslip angle. Using the linear lateral-directional dynamic equations, the under-actuated control mechanism was analyzed. The rudder could produce sideslip angle, and the roll angle could be controlled by sideslip angle. With the concept of cascade control, a controller of two levels was designed that was series connection of the roll angle controller and sideslip angle controller. Results show that the design of the lateral-directional cascade control strategy can stabilize the system and the tacking performance of the roll angle satisfies the requirement.
引用
收藏
页码:399 / 404
页数:6
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