Constrained Impulsive Trajectory Optimization for Orbit-to-Orbit Transfer
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
General Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55862
Reference40 articles.
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2. Accelerated gradient projection technique with application to rocket trajectory optimization
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4. Trajectory optimization for the Atlas/Centaur launch vehicle
5. A survey of impulsive trajectories.
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