Direct Approach for Computing Near-Optimal Low-Thrust Earth-Orbit Transfers
Author:
Affiliation:
1. University of Missouri–Columbia, Kansas City, Missouri 64110
2. NYMA, Inc., Brookpark, Ohio 44142
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3360
Reference7 articles.
1. Optimal low-thrust transfers to synchronous orbit
2. Designing continuous-thrust low-Earth-orbit to geosynchronous-Earth-orbit transfers
3. Optimum low thrust transfer to geosynchronous orbit
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