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高速再入飞行器跟踪制导方法对比研究

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针对标准再入轨迹跟踪制导问题,比较研究如何选取控制方法.采用Radau伪谱法由标准迎角方案、过程约束和飞行任务性能指标优化得到标准再入轨迹;分别以LQR控制和滑模控制建立纵向轨迹跟踪制导的控制模型,采用倾侧角反转策略作为横向制导方法,得到两种轨迹跟踪制导控制器.仿真结果表明,基于考虑模型或参数不确定性滑模控制的轨迹跟踪制导控制器鲁棒性较好,模拟试验成功率较高.
Comparative research on tracking guidance methods for high-speed reentry vehicles
To solve the problem of standard reentry trajectory tracking guidance,comparison and study have been conducted on how to choose the control method.The standard reentry trajectory is obtained by using the Radau pseudo spectral method in accordance with the standard angle of attack scheme,process constraints and flight mission performance index.The control model of longitudinal trajectory tracking guidance is established by adopting LQR control and sliding mode control respec-tively.The tilt angle inversion strategy is employed as a lateral guidance method obtaining two traj-ectory tracking guidance controllers.The simulation results indicate that the trajectory tracking guid-ance controllers possess better robustness,which are developed based on sliding mode control with model or parameter uncertainty considered,resulting in higher success rate of simulation test.

reentry guidancestandard trajectory guidance methodpseudo spectral method

张天佑、陈万春、周韬

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北京航空航天大学宇航学院,北京 102206

航天器设计优化与动态模拟技术教育部重点实验室,北京 100191

再入制导 标准轨迹制导法 伪谱法

2024

飞行力学
中国飞行试验研究院

飞行力学

CSTPCD北大核心
影响因子:0.37
ISSN:1002-0853
年,卷(期):2024.42(5)