Initial orbit determination method of maneuvering target based on prior knowledge
Author:
Affiliation:
1. Aerospace Engineering University,Beijing,China
2. National Innovation Institute of Defense Technology,Beijing,China
3. The Unit 63615 of People’s Liberation Army,Korla,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10280773/10281200/10281289.pdf?arnumber=10281289
Reference27 articles.
1. A Multimodal Differential Evolution Algorithm in Initial Orbit Determination for a Space-Based Too Short Arc
2. Study on evolutionary algorithms for initial orbit determination of near-earth asteroids with too-short-arc [J];li;Chinese Journal of Theoretical and Applied Mechanics,2021
3. Simulation & validation of ground-based optical-telescope imagingon target craft[J];han;Infrared and Laser Engineering,2019
4. Differential Evolution for Multimodal Optimization With Species by Nearest-Better Clustering
5. Particle swarm optimization for initial orbit determination with too-short-arc[J];li;Journal of Spacecraft TT&C Tecnology,2015
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