Autonomous Lunar Orbit Rendezvous Guidance Based on -Perturbed State Transition Matrix
Journal of Guidance, Control, and Dynamics ; 38 , 2 ; 315-322
2015-02-01
Article (Journal)
Electronic Resource
English
Autonomous Lunar Orbit Rendezvous Guidance Based on J2-Perturbed State Transition Matrix
Online Contents | 2015
|Rapid forecasting method for lunar orbit rendezvous guidance
European Patent Office | 2022
|Remote guidance rapid iterative guidance method for lunar orbit rendezvous
European Patent Office | 2025
|NTRS | 1962
|Engineering Index Backfile | 1962
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