General formulation for N-body tethered satellite system dynamics
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2K6, Canada
2. University of British Columbia, Vancouver, British Columbia V6T1Z4, 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/10.2514/3.21582
Reference12 articles.
1. A three-mass tethered system for micro-g/variable-g applications
2. Attitude dynamics of three-body tethered systems
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