Geometric Attitude Motion Planning for Spacecraft with Pointing and Actuator Constraints
Author:
Affiliation:
1. Politecnico di Milano, 20156 Milan, Italy
2. University of Strathclyde, Glasgow, Scotland G1 1XJ, United Kingdom
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.G001514
Reference8 articles.
1. Attitude Commands Avoiding Bright Objects and Maintaining Communication with Ground Station
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4. Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method
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