Hybrid thrusters and reaction wheels strategy for large angle rapid reorientation with high precision

Author:

Ye Dong,Sun Zhaowei,Wu Shunan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Robust tracking control design for spacecraft under control input saturation;Boskovic;J. Guidance Control Dyn.,2004

2. Robust adaptive variable structure control of spacecraft under control input saturation;Boskovic;J. Guidance Control Dyn.,2001

3. M.D. Tandale, K. Subbarao, J. Valasek, M.R. Akella, Structured adaptive model inversion control with actuator saturation constraints applied to tracking spacecraft maneuvers, in: Proceedings of the 2004 American Control Conference, vol. 1032, 2004, pp. 1031–1036.

4. Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances;Wallsgrove;J. Guidance Control Dyn.,2005

5. Time optimal attitude maneuver strategies for the agile spacecraft with reaction wheels and thrusters;Lee;J. Mech. Sci. Technol.,2005

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