Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft

CHEN Cheng; LIU Xiang

doi:10.21656/1000-0887.450094

Volume 46 Issue 3

Mar. 2025

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Article Navigation > Applied Mathematics and Mechanics > 2025 > 46(3): 283-297

CHEN Cheng, LIU Xiang. Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft[J]. Applied Mathematics and Mechanics, 2025, 46(3): 283-297. doi: 10.21656/1000-0887.450094

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Rigid-Flexible-Thermal Coupling Dynamic Modeling and Hybrid Control of Membrane Antenna Spacecraft

doi: 10.21656/1000-0887.450094

CHEN Cheng^1
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LIU Xiang^{1, 2
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1.
Department of Engineering Mechanics, Shanghai Jiao Tong University, Shanghai 200240, P.R.China
2.
Chongqing Research Institute, Shanghai Jiao Tong University, Chongqing 401122, P.R.China

Received Date: 2024-04-11
Rev Recd Date: 2024-05-09
Publish Date: 2025-03-01

Abstract

Abstract

Large space membrane antenna has a great prospect in the fields of deep space exploration, space-based early warning and earth observation. Due to the large-size and high-flexibility of the membrane structure, the membrane antenna spacecraft poses challenging dynamic and control issues. Meanwhile, to maintain the working performance of the antenna, the pointing accuracy and surface accuracy must be kept strictly. Therefore, accurate dynamic modeling and effective active control of large membrane antenna are of great significance and practical interest, and attract a lot of attentions in recent years. The rigid-flexible-coupling dynamics and hybrid control of membrane antenna spacecraft were studied. First, based on the nonlinear finite method the nonlinear dynamic model for the membrane antenna structure was established, and the nonlinear dynamic model order reduction was also studied. Then, in view of the thermal flux, the rigid-flexible-thermal coupling dynamic model for the spacecraft was established by means of the hybrid coordinate method. With the component synthesis vibration suppression method and the cable-actuator-based nonlinear vibration control method, a hybrid control system was designed to control the attitude motion meanwhile reduce the nonlinear vibration.
- membrane antenna,
- rigid-flexible-thermal coupling dynamic modeling,
- nonlinear vibration,
- hybrid control

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References(17)

References

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