Sinusoidal Path Planning for Attitude Maneuver of Flexible Spacecraft

Xiao Wen Wu; Lin Zhao; Yong Hao; Bo Zhang; Shuai Chen

doi:10.4028/www.scientific.net/AMM.532.187

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 532Sinusoidal Path Planning for Attitude Maneuver of...

Sinusoidal Path Planning for Attitude Maneuver of Flexible Spacecraft

Abstract:

Considering the complex of space environment, the influence of flexible attachments, the restraint of measurement and control precision, it makes difficult to control the attitude precisely. In order to improve the attitude maneuver's rapidity and its stability, this paper studied the attitude maneuver's path programming method of satellite with the flexible attachments. Through the establishment of the dynamic model of flexible satellites, and using multi-objective optimization algorithm to select the optimal parameter, an asymmetric sinusoidal maneuver path was planned. Simulation results show that the planned path could suppress flexible appendages vibration which brought by attitude changes, then the effectiveness of the planning algorithm is demonstrated.

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Periodical:

Applied Mechanics and Materials (Volume 532)

Pages:

187-190

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.532.187

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Online since:

February 2014

Authors:

Xiao Wen Wu*, Lin Zhao, Yong Hao, Bo Zhang, Shuai Chen

Keywords:

Attitude Maneuver, Flexible Vibration, Multi-Objective Optimization (MOP), Path Planning

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