Accession Number : AD0282706

Title :   TECHNIQUES FOR ANALYSIS OF NONLINEAR ATTITUDE CONTROL SYSTEMS FOR SPACE VEHICLES. VOLUME III. EXAMPLES OF ANALYTICAL DESIGN OF SPACECRAFT ATTITUDE CONTROL SYSTEMS

Corporate Author : TRW SPACE TECHNOLOGY LABS REDONDO BEACH CALIF

Personal Author(s) : ERGIN,E.I. ; NORUM,V.D. ; WINDEKNECHT,T.G.

Report Date : JUN 1962

Pagination or Media Count : 1

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

Descriptors :   *SATELLITES (ARTIFICIAL), *SPACECRAFT, CONTROL, DESIGN, ORBITS, SOLAR CELLS, SOLAR RADIATION, SPINNING(MOTION), STABILITY, TORQUE, VELOCITY

Distribution Statement : APPROVED FOR PUBLIC RELEASE