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Moments of inclination error distribution computer programA FORTRAN coded computer program is described which calculates orbital inclination error statistics using a closed-form solution. This solution uses a data base of trajectory errors from actual flights to predict the orbital inclination error statistics. The Scott flight history data base consists of orbit insertion errors in the trajectory parameters - altitude, velocity, flight path angle, flight azimuth, latitude and longitude. The methods used to generate the error statistics are of general interest since they have other applications. Program theory, user instructions, output definitions, subroutine descriptions and detailed FORTRAN coding information are included.
Document ID
19840021432
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Myler, T. R. (Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Publication Information
Publisher: NASA. Langley Research Center
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-165824
NAS 1.26:165824
Accession Number
84N29501
Funding Number(s)
CONTRACT_GRANT: NAS1-15000
PROJECT: RTOP 490-02-02-77-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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