Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tsukuba 305-8505, Japan
2. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
3. University of Tokyo, Tokyo 113-8654, Japan
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.G001750
Reference13 articles.
1. Flight status of IKAROS deep space solar sail demonstrator
2. Generalized Attitude Model for Spinning Solar Sail Spacecraft
3. Solar Sail Dynamics and Coning Control in Circular Orbits
4. Stability of Spinning Solar Sail-craft Containing A Huge Membrane
5. Spin Stability Criteria for Axisymmetric Spinning Body with Large Flexible Membrane
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