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A two-level trajectory decomposition algorithm featuring optimal intermediate target selectionA decomposition algorithm is presented which optimizes complex missions by partitioning the trajectory into natural segments such as ascent or entry. Each segment defines a full-rank targeting subproblem. These are solved sequentially using the Newton-Raphson algorithm. The master problem, representing the complete mission, is to determine subproblem targets and master-problem controls that optimize the mission objective subject to intersegment constraints. The gradient projection algorithm solves this problem using derivatives obtained analytically from finite-difference subproblem sensitivities. Thus, the mission is optimized by coordinating the solution of tractible subproblems. Computational results for a synchronous equatorial mission are included.
Document ID
19780027940
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Petersen, F. M.
(Martin Marietta Aerospace Denver, CO, United States)
Cornick, D. E.
(Martin Marietta Aerospace Denver, CO, United States)
Brauer, G. L.
(Martin Marietta Aerospace Denver, Colo., United States)
Rehder, J. R.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1977
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 14
Subject Category
Astrodynamics
Accession Number
78A11849
Funding Number(s)
CONTRACT_GRANT: NAS1-13611
Distribution Limits
Public
Copyright
Other

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