Dynamics of a spacecraft with large flexible appendage constrained by multi-strut passive damper

Author:

Jia Ying-Hong,Xu Shi-Jie,Hu Quan

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference22 articles.

1. Iyer, A., Singh, S. N.: Variable structure slewing control and vibration damping of flexible spacecraft. Acta Astronautica 25, 1–9 (1991)

2. Oz, H. O., Mostafa, O.: Variable structure control systems maneuvering of flexible spacecraft. Journal of the Astronautical Sciences 36, 311–344 (1988)

3. Nayeri, M. R. D., Alasty, A., Daneshjou, K.: Neural optimal control of flexible spacecraft slew maneuver. Acta Astronautica 55, 817–827 (2004)

4. Xin, M., Pan, H. J.: Integrated control of position, attitude, and flexible motion for satellite proximity operations. In: AIAA Guidance, Navigation, and Control Conference, Chicago, Illinois, USA, 1–19 (2009)

5. Maly, J. R., Anandakrishnan, S. M., Pendleton, S. C., et al.: Flight hardware for the Hubble Space Telescope solar array damper. In: Proceedings of SPIE, Newport Beach, CA 3989, 14–25 (2000)

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