Attitude Responses in Coupled Orbit-Attitude Dynamical Model in Earth–Moon Lyapunov Orbits
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Armstrong Hall of Engineering, Purdue University, West Lafayette, Indiana 47907-2045
2. Department of Aerospace Engineering, Politecnico di Milano, 20156 Milan, Italy
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.G000469
Reference17 articles.
1. Attitude Stability of a Spinning Satellite in an Elliptic Orbit
2. Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem
3. The restricted problem of three bodies with rigid dumb-bell satellite
4. Attitude stability of a rigid body placed at an equilibrium point in the restricted problem of three bodies
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