A THREE-DIMENSIONAL LIFTING REENTRY VEHICLE SIMULATION
Abstract
The three-dimensional equations of motion, written in a flight path coordinate system, are presented for a re-entering orbital vehicle. An analog computer circuit used for the solution of these equations is described. Typical computer solutions are presented and discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1962
- Accession Number
- AD0289524
Entities
People
- Norbert D. Lavally
Organizations
- Air Force Institute of Technology