A New Strategy of Guidance Command Generation for Re-entry Vehicle

被引:1
|
作者
Xie DaoCheng [1 ]
Wang ZhongWei [1 ]
Zhang WeiHua [1 ]
机构
[1] Natl Univ Def Technol, Changsha 410073, Hunan, Peoples R China
基金
国家高技术研究发展计划(863计划);
关键词
Re-entry homing vehicle; radar seeker; attack angle; sideslip angle; Euler angles; transformation matrix;
D O I
10.14429/dsj.63.2360
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Guidance command for re-entry vehicle can be in lots of formats, but the Euler angles can be provided directly by gyros, so designers used to develop autopilot with commands of Euler angles. After the generation of commands of attack angle and sideslip angle, it's important to settle how to convert commands of attack angle and sideslip angle to commands of Euler angles. Traditional conversion strategy relies on bank angle, solution to bank angle comprises complicated calculation and can't be precise. This paper introduces a new conversion strategy of guidance command This strategy relies on the relative position and velocity measured by seeker, an auxiliary coordinate is established as a transition, the transformation matrix from launch coordinate to body coordinate is solved in a new way, then the commands of Euler angles are obtained. The calculation of bank angle is avoided. The autopilot designed with the converted Euler-angle commands, can track commands of attack angle and sideslip angle steadily. The vehicle reaches the target point precisely. Simulation results show that the new conversion strategy based on seeker information from commands of attack angle and sideslip angle to Euler-angle commands is right.
引用
收藏
页码:93 / 100
页数:8
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