TECHNIQUES FOR ANALYSIS OF NONLINEAR ATTITUDE CONTROL SYSTEMS FOR SPACE VEHICLES. VOLUME III. EXAMPLES OF ANALYTICAL DESIGN OF SPACECRAFT ATTITUDE CONTROL SYSTEMS
Abstract
Contents: The rate diagram technique in analysis and design of space v icle on-off attitude control systems A simple system for sun orientation of a pinning satellite Design con iderations of inertia wheel systems for attitude control of satellite vehicles
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1962
- Accession Number
- AD0282706
Entities
People
- E.i. Ergin
- T.g. Windeknecht
- V.d. Norum