Optimal multi-objective low-thrust spacecraft trajectories
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Publication:1574399
DOI10.1016/S0045-7825(99)00393-XzbMath0956.70020MaRDI QIDQ1574399
J. W. Hartmann, V. Coverstone-Carroll, W. J. Mason
Publication date: 12 March 2001
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
multi-objective genetic algorithmhybrid optimization methodEarth-Mars missionEarth-Mercury missionlow-thrust trajectory optimizerPareto optimal trajectories
Related Items (8)
A systematic review on the advancement in the study of fuzzy variational problems ⋮ A multi-objective approach to the design of low thrust space trajectories using optimal control ⋮ Station keeping of constellations using multiobjective strategies ⋮ MOMPA: multi-objective marine predator algorithm ⋮ Near optimal re-entry guidance law using inverse problem approach ⋮ Numerical and analytical study of optimal low-thrust limited-power transfers between close circular coplanar orbits ⋮ Pareto frontier for the time-energy cost vector to an Earth-Moon transfer orbit using the patched-conic approximation ⋮ Optimization of low-thrust limited-power trajectories in a noncentral gravity field-transfers between orbits with small eccentricities
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