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A multiple-impulse function for orbital transfer and its derivativesA multiple-impulse function is represented as a sequence of single-impulse functions. The single-impulse transfer which yields the velocity change required to transfer from a specified initial orbit to a partially specified final orbit is developed. Analytic derivatives of the function are obtained for use in optimization techniques. A four-impulse transfer is outlined. The analytic derivatives may allow more efficient optimization than numerical derivatives do.
Document ID
19720012221
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kibler, J. F.
(NASA Langley Research Center Hampton, VA, United States)
Hoffman, L. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Space Sciences
Report/Patent Number
L-8106
NASA-TM-X-2492
Report Number: L-8106
Report Number: NASA-TM-X-2492
Accession Number
72N19871
Funding Number(s)
PROJECT: RTOP 815-00-00-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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