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A two-level trajectory decomposition algorithm featuring optimal intermediate target selectionA decomposition algorithm is presented that 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
19760028331
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
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 8, 2013
Publication Date
July 1, 1975
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 75-054
Meeting Information
Meeting: Astrodynamics Specialist Conference
Location: Nassau
Country: Bahamas
Start Date: July 28, 1975
End Date: July 30, 1975
Sponsors: American Astronautical Society and American Institute of Aeronautics and Astronautics
Accession Number
76A11297
Funding Number(s)
CONTRACT_GRANT: NAS1-13611
Distribution Limits
Public
Copyright
Other

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