Optimal Guidance of Low-Thrust Interplanetary Space Vehicles

Optimal Guidance of Low-Thrust Interplanetary Space Vehicles

The low-thrust guidance problem is defined as the minimum terminal variance (MTV) control of a space vehicle subjected to random perturbations of its trajectory. To accomplish this control task, only bounded thrust level and thrust angle deviations are allowed, and these must be calculated based sol...

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Bibliographic Details
Main Author: Ash, Gerald Richard
Format: Others
Published: 1969
Online Access:https://thesis.library.caltech.edu/8085/1/Ash_gr_1969.pdf
Ash, Gerald Richard (1969) Optimal Guidance of Low-Thrust Interplanetary Space Vehicles. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/RDY0-PH47. https://resolver.caltech.edu/CaltechTHESIS:02192014-095711728 <https://resolver.caltech.edu/CaltechTHESIS:02192014-095711728>

Internet

https://thesis.library.caltech.edu/8085/1/Ash_gr_1969.pdf
Ash, Gerald Richard (1969) Optimal Guidance of Low-Thrust Interplanetary Space Vehicles. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/RDY0-PH47. https://resolver.caltech.edu/CaltechTHESIS:02192014-095711728 <https://resolver.caltech.edu/CaltechTHESIS:02192014-095711728>

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