Relationships Between Maneuver Time and Energy for Reaction Wheel Attitude Control
Author:
Affiliation:
1. University of California, Santa Cruz, Santa Cruz, California 95064
2. Naval Postgraduate School, Monterey, California 93943
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G002843
Reference27 articles.
1. Survey of time-optimal attitude maneuvers
2. Time-optimal three-axis reorientation of a rigid spacecraft
3. Time-Optimal Control of Axisymmetric Rigid Spacecraft Using Two Controls
4. FlemingA. “Real-Time Optimal Slew Maneuver Design and Control,” M.S. Thesis, Naval Postgraduate School, Monterey, CA, 2004.
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