Fast Trajectory Deviation Prediction Algorithm with Arbitrary Degree/Order Gravitational Potential
Author:
Affiliation:
1. National University of Defense Technology, 430014 Wuhan, People’s Republic of China
2. National University of Defense Technology, 410073 Changsha, People’s Republic of China
Funder
National Basic Research Program 973 of China
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G003734
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5. Second-order solution of artificial satellite theory without air drag
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