Comment on "Time-Optimal Orbit Transfer Trajectory for Solar Sail Spacecraft"
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
2. California Institute of Technology, Pasadena, Calif.
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/10.2514/3.56160
Reference19 articles.
1. Feedforward control to track the output of a forced model
2. On the stability of solutions to minimal and nonminimal design problems
3. AIAA 82-4083
4. Time-optimal orbit transfer trajectory for solar sail spacecraft
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