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Simple control laws for continuous-thrust escape or capture and their use in optimisationInterplanetary missions which use low-thrust, high specific impulse propulsion can further capitalise on the capabilities of the propulsion system by using it to effect escape from the launch body or capture at a target body.
Document ID
20060029665
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Petropoulos, A. E.
Whiffen, G. J.
Sims, J. A.
Date Acquired
August 23, 2013
Publication Date
August 5, 2002
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
low-thrust escape low-thrust capture optimal spiral escape

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