Optimal Continuous-Thrust Rephasing Maneuver in Circular Orbit

Author:

Gonzalo Juan L.1,Bombardelli Claudio1

Affiliation:

1. Technical University of Madrid-UPM, 28040 Madrid, Spain

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference15 articles.

1. Autonomous Constellation Maintenance

2. Ion Beam Shepherd for Contactless Space Debris Removal

3. Optimal Multi-Objective Linearized Impulsive Rendezvous

4. LawdenD. F., Optimal Trajectories for Space Navigation, Butterworths, London, 1963, pp. 54–69.

5. MarecJ.P., Optimal Space Trajectories, Vol. 1, Elsevier, New York, 2012, pp. 155–225.

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2. Spacecraft Rendezvous in Closed Keplerian Orbits Using Constant Radial Thrust Acceleration;Journal of Guidance, Control, and Dynamics;2023-06

3. Atlas of Optimal Low-Thrust Rephasing Solutions in Circular Orbit;Journal of Guidance, Control, and Dynamics;2023-05

4. Orbital Rendezvous via a General Nonsingular Method;Journal of Guidance, Control, and Dynamics;2022-01

5. Optimal Constant-Thrust Radius Change in Circular Orbit;Journal of Guidance, Control, and Dynamics;2019-08

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