Direct Path Method for Flexible Multibody Spacecraft Dynamics
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57167
Reference17 articles.
1. Dynamics Analysis of a Two-Body Gravitationally Oriented Satellite
2. A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom
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