Electric thruster mode-pruning strategies for trajectory-propulsion co-optimization
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DOI: 10.1016/j.ast.2021.106828
Abstract: Abstract Application of idealized constant-specific-impulse, constant-thrust electric thruster performance models or curve-fitted polynomials is quite common for spacecraft trajectory design. However, incorporation of realistic performance models of multi-mode electric thrusters leads to notable challenges, and… read more here.
Keywords: optimization; thruster mode; electric thruster; thruster ... See more keywords