Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles

被引:1
|
作者
Tan, Shujun [1 ,2 ]
Zhao, Wang [2 ]
Liu, Jinfan [3 ]
Mao, Yuming [3 ]
机构
[1] Dalian Univ Technol, State Key Lab Struct Anal Optimizat & CAE Software, Dalian 116024, Peoples R China
[2] Dalian Univ Technol, Key Lab Adv Technol Aerosp Vehicles Liaoning Prov, Dalian 116024, Peoples R China
[3] Shanghai Aerosp Syst Engn Inst, Shanghai 201109, Peoples R China
基金
中国国家自然科学基金;
关键词
Pogo vibration; Model reduction; Active control; Launch vehicle; Adaptive control; STABILITY ANALYSIS; ROCKETS; VIBRATION;
D O I
10.1016/j.actaastro.2023.02.004
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In order to better solve the problem of Pogo stability considering parameter uncertainty and time-variation in the large launch vehicle, the model-reference adaptive control based on the dimensionality reduction model (MRAC-DRM) is proposed. Firstly, the state space Pogo model with an active controller is established for control system design by the improved Rubin method. Secondly, a greatly reduced dimensional model of the Pogo control system is derived from the eigenvalue transformation theory, which preserves the features of Pogo instability and is appropriate for control design. Then, the reference model and adaptive control law are designed by the model -reference adaptive control method based on the reduced dimensional model. Finally, two examples with different types of propulsion systems are used to demonstrate the effectiveness of the proposed MRAC-DRM. Simulation results demonstrate that the proposed method not only has excellent adaptability to the Pogo systems with parameter uncertainty and time-variation but also is insensitive to the initial value of feedback gain.
引用
收藏
页码:43 / 56
页数:14
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