A Powered Flight Six-Degree-of-Freedom Trajectory Program for Vehicles with Freely Spinning Tail Stabilizers,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 30, 1969
- Accession Number
- AD0863644
Entities
People
- John E. Holmes
Organizations
- Naval Ordnance Laboratory