Utilizing A Genetic Algorithm for Optimization of Two-Impulse Rendezvous Maneuvers Between Spacecraft in the Martian Orbit
Author:
Affiliation:
1. SSAU,Department of Flight Dynamics and Control Systems,Samara,Russia,443086
2. SSAU,Department of Higher Mathematics,Samara,Russia,443086
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10349345/10349369/10349672.pdf?arnumber=10349672
Reference12 articles.
1. Terminal Guidance System for Satellite Rendezvous
2. A Geometrical, Reachable Set Approach for Constrained Pursuit–Evasion Games with Multiple Pursuers and Evaders
3. Optimal On-Orbit Inspection of Satellite Formation
4. Time-optimal maneuvers of a spacecraft between two arbitrary states in proximity of a circular reference orbit
5. Autonomous Satellite Rendezvous and Proximity Operations with Time-Constrained Sub-Optimal Model Predictive Control
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