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  • 1
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    Moments of inclination error distribution computer program (1981)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A 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.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-CR-165824 , NAS 1.26:165824
    Format: application/pdf
    Location Call Number Expected Availability
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