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杨春宁, 方家为, 李春, 葛晖
1.浙江大学 航空航天学院,浙江 杭州 310027
2.上海航天控制技术研究所,上海 201109
Hypersonic vehicle blended control methodology based on stability criterion
YANG Chun ning, FANG Jia wei, LI Chun, GE Hui
1.School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China;
2. Shanghai Institute of Spaceflight Control Technology, Shanghai 201109, China
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The traditional strategy to open the side jet in blended control system was strongly dependent on priori data, which led to poor robustness, therefore, a blended control methodology based on stability criterion was proposed. According to hypersonic vehicle model, the stability criterion was deduced to predict the vehicle stability. When the vehicle was nearly unstable, side force moment was added by opening the side jet engines to control the vehicle. This method does not rely on priori data, and it can ensure the steady flight and high maneuverability in high Mach flight. The full state six-degrees of freedom hypersonic vehicle model was established to finish the simulation, results indicate that the proposed method has better performance on disturbance rejection, and is more robust than traditional control strategy.
出版日期: 2017-03-06
CLC:  V 249.122  


作者简介: 杨春宁(1970—),男,副研究员,从事飞行器建模与控制等研究. ORCID: 0000-0001-7225-4286. E-mail:
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杨春宁, 方家为, 李春, 葛晖. 基于稳定性判据的高超声速复合控制方法[J]. 浙江大学学报(工学版), 10.3785/j.issn.1008-973X.2017.02.027.

YANG Chun ning, FANG Jia wei, LI Chun, GE Hui. Hypersonic vehicle blended control methodology based on stability criterion. JOURNAL OF ZHEJIANG UNIVERSITY (ENGINEERING SCIENCE), 10.3785/j.issn.1008-973X.2017.02.027.

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