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Primer vector theory and applicationsA method developed to compute two-body, optimal, N-impulse trajectories was presented. The necessary conditions established define the gradient structure of the primer vector and its derivative for any set of boundary conditions and any number of impulses. Inequality constraints, a conjugate gradient iterator technique, and the use of a penalty function were also discussed.
Document ID
19760004112
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Jezewski, D. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Astrodynamics
Report/Patent Number
JSC-S-439
NASA-TR-R-454
Accession Number
76N11200
Funding Number(s)
PROJECT: RTOP 986-16-20-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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