NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Computing Optimal Multiarc TrajectoriesOptimal Multi-Arc Trajectories (OMAT) computer program designed to calculate solution to optimal-trajectory problem in cases of low thrust-to-weight ratios. Developed for two-body exoatmospheric problem with three degrees of freedom in inverse-square force field. Offers two different options: impulsive changes in velocity and finite burns with low thrust-to-weight ratios. Two distinct solutions available from program: optimal multi-impulse (OMI) solution and optimal multiburn (OMB) solution. Two solutions obtained separately, or results of OMI solution used to guess unknown parameters of OMB solution. Written for DEC VAX-series computer. Written completely in FORTRAN 77.
Document ID
19890000411
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jezewski, Donald J.
(McDonnell-Douglas Corp.)
Date Acquired
August 14, 2013
Publication Date
August 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 8
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MSC-21112
Report Number: MSC-21112
ISSN: 0145-319X
Accession Number
89B10411
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available