A SIX-DEGREE-OF-FREEDOM DIGITAL COMPUTER PROGRAM FOR TRAJECTORY SIMULATION
Abstract
A documentation of a six-degree-of-freedom model for digital simulation of the trajectory of an unguided, fin-stabilized, wind-sensitive rocket is presented. This model was developed by the Atmospheric Sciences Laboratory, White Sands Missile Range, New Mexico, to study both theoretical and empirical performance characteristics of unguided rockets. The basic equations of motion and their mathematical formulation for this model are presented without derivation. A general flow chart, a listing of the program, a list of the principal flads used, and a listing of a typical input data deck are included.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1967
- Accession Number
- AD0664116
Entities
People
- Bernard F. Engebos
- Louis D. Duncan
Organizations
- Atmospheric Sciences Laboratory