Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Problem Formulation

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Report Number: FDL TDR 64-1 Part 1 Volume 1
Author(s): Brown, Robert C., Brulle, Robert V., Combs, A. E., Griffin, Gerald D.
Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Pages: 202
Contract: AF 33(657)-8829
DoD Project: 1431
DoD Task: 143103
Identifier: AD0452592

Abstract:
A trajectory computation program is described for determining vehicle performance throughout the entire flight regime of speed and altitude in the atmosphere and gravity field of a nonspherical rotating planet. The program is formulated for seven options of varying refinement from the six-degree-of- freedom problem to the two-degree point mass problem. A reverse option for the aerodynamic analysis of flight test data, a punched card output, and a semiautomatic computational tie to an interplanetary trajectory computer program are included. The program is specifically oriented for computation on the IBM 7090/7094 digital computer using the FAP/FORTRAN2 machine language.

Provenance: AFRL/VACA

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