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Space Trajectory Error Analysis Program (STEAP) for halo orbit missions. Volume 2: Programmer's manualThe six month effort was responsible for the development, test, conversion, and documentation of computer software for the mission analysis of missions to halo orbits about libration points in the earth-sun system. The software consisting of two programs called NOMNAL and ERRAN is part of the Space Trajectories Error Analysis Programs. The program NOMNAL targets a transfer trajectory from earth on a given launch date to a specified halo orbit on a required arrival date. Either impulsive or finite thrust insertion maneuvers into halo orbit are permitted by the program. The transfer trajectory is consistent with a realistic launch profile input by the user. The second program ERRAN conducts error analyses of the targeted transfer trajectory. Measurements including range, doppler, star-planet angles, and apparent planet diameter are processed in a Kalman-Schmidt filter to determine the trajectory knowledge uncertainty.
Document ID
19740018195
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Byrnes, D. V.
(Martin Marietta Aerospace Denver, CO, United States)
Carney, P. C.
(Martin Marietta Aerospace Denver, CO, United States)
Underwood, J. W.
(Martin Marietta Aerospace Denver, CO, United States)
Vogt, E. D.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Space Sciences
Report/Patent Number
MCR-74-98-VOL-2
NASA-CR-139021
Report Number: MCR-74-98-VOL-2
Report Number: NASA-CR-139021
Accession Number
74N26308
Funding Number(s)
CONTRACT_GRANT: NAS5-24067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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