Robustness Evaluation of Theta-D Technique for Spacecraft Attitude Control Subject to Reaction Wheel Failures
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[1] Mazen Alamir,et al. Further Results on the Controllability of a Two-Wheeled Satellite , 2007 .
[2] Youdan Kim,et al. Spin-Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels , 2001 .
[3] J. R. Cloutier,et al. The capabilities and art of state-dependent Riccati equation-based design , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).
[4] Ming Xin,et al. Preserving Spacecraft Attitude Control Accuracy Using -D Controller Subject to Reaction Wheel Failures , 2010 .
[5] Itzhak Barkana,et al. Direc t Adaptive Control Treatment to Flight Contro l Input Saturation , 2005 .
[6] Bryce A. Roberts,et al. FUSE in-orbit attitude control with two reaction wheels and no gyroscopes , 2003, SPIE Astronomical Telescopes + Instrumentation.
[7] Arthur E. Bryson,et al. Applied Optimal Control , 1969 .
[8] Ming Xin,et al. Libration point stationkeeping using the θ-D technique , 2008 .
[9] N. Harris McClamroch,et al. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators , 1993 .
[10] Jinho Kim,et al. A mixed-mode attitude control system strategy for actuator failure accommodation , 2001 .