Accession Number : AD0863644
Title : A Powered Flight Six-Degree-of-Freedom Trajectory Program for Vehicles with Freely Spinning Tail Stabilizers,
Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD
Personal Author(s) : Holmes, John E.
Report Date : 30 OCT 1969
Pagination or Media Count : 91
Abstract : This program provides for the simulation of powered six-degree-of-freedom trajectories over a spherical rotating earth for those vehicles which have a fore and aft section, which may or may not rotate at different spin rates, but, which rotate about a common longitudinal axis. The program does not permit any mass or inertial asymmetries, but it can be run using either a rolling or nonrolling vehicle axis system and a variable integration time step. (Author)
Descriptors : *COMPUTER PROGRAMS), (*BOMBS, BOMB TRAJECTORIES), (*BOMB TRAJECTORIES, EQUATIONS OF MOTION, AERODYNAMIC LOADING, MOMENTS, DAMPING, THRUST, SUBROUTINES, MATHEMATICAL MODELS, COMPUTER PROGRAMS.
Subject Categories : Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE