Academic Journal of Engineering and Technology Science, 2023, 6(2); doi: 10.25236/AJETS.2023.060207.
Wu Ping, Chen Haizhu, Tian Feng, Wang Jiachun
Bijie Industrial Polytechnic College, Bijie, Guizhou, 551700, China
Due to the improvement of the complexity and diversity of modern aviation work, there are more requirements for the large altitude posture, the maneuverability and the accuracy of the tracking direction of flexible satellite for observing and tracking the ground. In this context, this paper discusses the large inclination maneuver attitude control theory and stability method of flexible satellites, and designs a shape memory alloy compression release device, which is expected to be used as a reference for relevant workers.
flexible satellite; attitude maneuver; solar panel vibration; suppression
Wu Ping, Chen Haizhu, Tian Feng, Wang Jiachun. Research on Attitude Maneuver and Solar Panel Vibration Suppression of Flexible Satellite. Academic Journal of Engineering and Technology Science (2023) Vol. 6, Issue 2: 45-49. https://doi.org/10.25236/AJETS.2023.060207.
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