Vertical Ascent to Geosynchronous Orbit with Constrained Thrust Angle
Author:
Affiliation:
1. National Central University, Chungli 32054, Taiwan, Republic of China
2. Chung Shan Institute of Science and Technology, Lungtan 32526, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3527
Reference11 articles.
1. Vertical ascent to geosynchronous orbit
2. Optimal vertical ascent to GEO with thrust acceleration and dynamic pressure constraints
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