Rapid Trajectory Design for Low-Thrust Many-Revolution Rendezvous Using Analytical Derivations
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS（2025）
Key words
Orbital Elements,Earth Orbit Rendezvous,Argument of Latitude,Trajectory Optimization,Newton Raphson Method,Low Thrust Trajectory,Satellite Constellations,On-Orbit Servicing, Assembly, and Manufacturing,Astrodynamics
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