Tactical Missile Encounter (TAME) Simulation Computer Program. Volume 1. Analyst Manual.
Abstract
The two volumes of this document present an analyst manual and a users manual for a three dimensional, three degree-of-freedom trajectory simulation. The missile model described in this volume uses trimmed aerodynamic data (zero pitching moment) with the missile autopilot computations approximated in the steady state using a single time lag representation of the dynamic response. Several missile autopilot systems are approximated as are several target options. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1970
- Accession Number
- AD0872464
Entities
People
- Donald R. Peters
- Heywood Sobel
- Mont J. Stevens
- Robert D. Feldman
Organizations
- Hughes Aircraft Company