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Attitude profile design programThe Attitude Profile Design (APD) Program was designed to be used as a stand-alone addition to the Simplex Computation of Optimum Orbital Trajectories (SCOOT). The program uses information from a SCOOT output file and the user defined attitude profile to produce time histories of attitude, angular body rates, and accelerations. The APD program is written in standard FORTRAN77 and should be portable to any machine that has an appropriate compiler. The input and output are through formatted files. The program reads the basic flight data, such as the states of the vehicles, acceleration profiles, and burn information, from the SCOOT output file. The user inputs information about the desired attitude profile during coasts in a high level manner. The program then takes these high level commands and executes the maneuvers, outputting the desired information.
Document ID
19910020867
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Astrodynamics
Report/Patent Number
TR-91-NASA-37850-004
NASA-CR-184183
NAS 1.26:184183
Report Number: TR-91-NASA-37850-004
Report Number: NASA-CR-184183
Report Number: NAS 1.26:184183
Accession Number
91N30181
Funding Number(s)
CONTRACT_GRANT: NAS8-37850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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