Advancing primer vector theory for averaged two-body perturbed dynamics with eclipsing
Author:
Affiliation:
1. The University of Texas at Austin
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1279
Reference38 articles.
1. Low-Thrust Orbit Transfers Using Candidate Lyapunov Functions with a Mechanism for Coasting
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3. Rapid generation of low-thrust many-revolution earth-center trajectories based on analytical state-based control
4. Analytical Techniques for the Optimisation of Rocket Trajectories
5. A Survey on Low-Thrust Trajectory Optimization Approaches
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