Discrete Multiobjective Optimization Methodology applied to the Mixed Actuators Problem and Tested in a Hardware-in-the-loop Rendezvous Simulator
Author:
Affiliation:
1. National Institute for Space Research (INPE)
2. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1991
Reference40 articles.
1. Automated Rendezvous and Docking of Spacecraft
2. Comparative study of various control methods for attitude control of a LEO satellite
3. Tracking Rigid Body Motion Using Thrusters and Momentum Wheels
4. Three-axis Attitude Control with Two Reaction Wheels and Magnetic Torquer Bars
5. Contingency Mixed Actuator Controller Implementation for the Dawn Asteroid Rendezvous Spacecraft
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