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Low thrust orbit determination programLogical flow and guidelines are provided for the construction of a low thrust orbit determination computer program. The program, tentatively called FRACAS (filter response analysis for continuously accelerating spacecraft), is capable of generating a reference low thrust trajectory, performing a linear covariance analysis of guidance and navigation processes, and analyzing trajectory nonlinearities in Monte Carlo fashion. The choice of trajectory, guidance and navigation models has been made after extensive literature surveys and investigation of previous software. A key part of program design relied upon experience gained in developing and using Martin Marietta Aerospace programs: TOPSEP (Targeting/Optimization for Solar Electric Propulsion), GODSEP (Guidance and Orbit Determination for SEP) and SIMSEP (Simulation of SEP).
Document ID
19730009135
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hong, P. E.
(Martin Marietta Corp. Denver, CO, United States)
Shults, G. L.
(Martin Marietta Corp. Denver, CO, United States)
Huling, K. R.
(Martin Marietta Corp. Denver, CO, United States)
Ratliff, C. W.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1972
Subject Category
Space Sciences
Report/Patent Number
MCR-72-292
NASA-CR-112256
Report Number: MCR-72-292
Report Number: NASA-CR-112256
Accession Number
73N17862
Funding Number(s)
CONTRACT_GRANT: NAS1-11686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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