Nonlinear Input Shaping Control of Flexible Spacecraft Reorientation Maneuver
Author:
Affiliation:
1. University of British Columbia, Vancouver, British Columbia V6T 1W5, Canada
2. Canadian Space Agency, St.-Hubert, Quebec J3Y 8Y9, Canada
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/10.2514/2.4252
Reference27 articles.
1. Acceleration Profiles for Minimizing Residual Response
2. Minimizing Residual Vibration for Point-to-Point Motion
3. Shaped Torque Techniques
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