Assessment of a Dynamical Gyroscope Model Utilizing Digital Simulation Techniques
Abstract
This report presents an assessment and performance of a dynamical gyroscope modelled for a six-degree-of-freedom digital missile trajectory simulation. Mathematical models and digital simulation results of an idealized gyro model and the dynamical (realistic) model are given. The computer program listings are presented in the appendices. (AUthor)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 03, 1977
- Accession Number
- ADA042497
Entities
People
- Larry R. Murdock
Organizations
- United States Army Aviation and Missile Command