Optimal variable-thrust transfer of a power- limited rocket between neighboring circular orbits
Author:
Affiliation:
1. United Aircraft Corporation, East Hartford, Conn
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2281
Reference7 articles.
1. OPTIMAL LOW-THRUST NEAR-CIRCULAR ORBITAL TRANSFER
2. September 1963;Kelley H J
3. The Optimization of Trajectories
4. Terminal Guidance System for Satellite Rendezvous
5. Minimum Transfer Time for a Power-Limited Rocket
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