Slewing Flexible Spacecraft with Deflection-Limiting Input Shaping
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
2. Lockheed Palo Alto Research Laboratory, Palo Alto, California 94304
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/10.2514/2.4036
Reference29 articles.
1. Near-minimum time, closed-loop slewing of flexible spacecraft
2. Near-minimum-time control of distributed parameter systems - Analytical and experimental results
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4. Shaped Torque Techniques
5. Optimal Large-Angle Single-Axis Rotational Maneuvers of Flexible Spacecraft
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