DESIGN CONCEPT FOR THE ST-323 STABILIZED PLATFORM,
Abstract
A study has been made at the Army Inertial Guidance and Control Laboratory to determine design characteristics required for advanced systems requiring inertial guidance. These requirements have been utilized with state-ofthe-art instrument technology to produce the design concept for the ST-323 stabilized platform whose design also includes Army test philosophy as well as performance requirements. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 27, 1963
- Accession Number
- AD0426352
Entities
People
- Wilbur E. Grunwald
Organizations
- United States Army Aviation and Missile Command