First Flight Results on Time-Optimal Spacecraft Slews
Author:
Affiliation:
1. Naval Postgraduate School, Monterey, California 93943
2. Charles Stark Draper Laboratory, Inc., Houston, Texas 77058
3. Leffler Consulting, LLC, Chantilly, Virginia 20151
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
http://arc.aiaa.org/doi/pdf/10.2514/1.54937
Reference34 articles.
1. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints
2. Near-minimum-time eigenaxis rotation maneuvers using reaction wheels
3. Large angle attitude control of spacecraft with actuator saturation
4. Time-optimal three-axis reorientation of a rigid spacecraft
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