Abstract This chapter presents a method to determine fuel-optimal trajectories for satellite formation maneuver using low-thrust continuous propulsion.
Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation
25.10.2016
28 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Trajectory Optimization , Nonlinear Programming Problem , Satellite Formation , Formation Maneuver , Trajectory Optimization Problem Engineering , Control, Robotics, Mechatronics , Calculus of Variations and Optimal Control; Optimization , Aerospace Technology and Astronautics , Fluid- and Aerodynamics
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|Approximate finite-thrust trajectory optimization.
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