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- W2070926511 abstract "The minimum-time, constant-thrust, orbital phasing maneuver is studied numerically. Nondimensionalization reduces the problem to one where thrust magnitude and phase angle are the only parameters. Extremal solutions are obtained for the entire range of practical values of thrust magnitude and phase angle. Plots of trajectories, thrust-angle proe les, and loci of initial costates are used to identify a near-invariance principle that leads to a variety of conclusions about this class of problems. The types of thrust-angle proe les are shown to fall into at least four types, two of which exist within the region of near-invariance. These two thrust-angle proe le types are distinguished by thetime-of-e ight tf, andthetransition between them takesplacefora tf of approximately one-half of an orbit. The relationship between tf and the ratio of thrust to phase angle is also shown to be nearly invariant over a wide range of thrust magnitudes." @default.
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- W2070926511 date "2003-11-01" @default.
- W2070926511 modified "2023-09-25" @default.
- W2070926511 title "Minimum-Time Orbital Phasing Maneuvers" @default.
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- W2070926511 doi "https://doi.org/10.2514/2.6921" @default.
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