VSCMG System Model Based on Euler Kinematics Equation

Author:

Guan Rongqiang,Li Cong,Lv Qiongying

Publisher

Springer Nature Singapore

Reference11 articles.

1. Ford KA, Hall CD (1997) Flexible spacecraft reorientations using gimbaled momentum wheels. In: Proceedings of the 1997 AAS/AIAA astrodynamics conference, 4–7 Aug 1997, Sun Valley, Idaho. AIAA, Reston, pp 1895–1913

2. David JR, Panagiotis T, Jerry LF (2001) Variable speed control moment gyroscope workbench: a new simulation tool for tomorrow’s spacecraft. In: The 20th digital avionics systems conference, 14–18

3. Yoon H, Tsiotras P (2004) Singularity analysis of variable-speed control moment gyros—part I: no power constraint case. In: Collection of technical papers-AIAA/AAS astrodynamics specialist conference, pp 955–970

4. Bruccoleri C, Lee D-J, Mortari D (2005) Single-point optimal attitude determination using modified Rodrigues parameters. In: AAS Malcolm D. Shuster astronautics symposium 05-459

5. Hall CD (1997) Momentum transfer dynamics of a gyrostat with a discrete damper. J Guid Control Dyn 20(6):1072–1075

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