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Techniques for analysis of nonlinear attitude control systems. Vol. 1. Characteristics of the spacecraft attitude control problem

Autore: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.); Space Technology Laboratories, inc.
Editore: Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962.
Serie: Aeronautical Systems Division (U.S.).; Technical Documentary Report
Edizione/Formato:   book_printbook : National government publication : English
Banca dati:WorldCat
Sommario:
This four volume report was prepared in order to compile, describe, and apply available nonlinear analysis and design techniques for space vehicle attitude control systems and to outline additional areas of future effort to improve present analysis and design procedures. Each of the four volumes is relatively independent of the others. Volume I is a definition and description of the problems associated with the  Per saperne di più…
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Tipo materiale: Government publication, National government publication
Tipo documento: Book
Tutti gli autori / Collaboratori: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.); Space Technology Laboratories, inc.
Numero OCLC: 444644271
Note: "June 1962."
AD0282057 (from http://www.dtic.mil).
Research supported by the United States Air Force, Air Force Systems Command, and performed by Space Technology Laboratories, Inc.
Descrizione: viii, 90 pages : illustrations ; 28 cm.
Titolo della serie: Aeronautical Systems Division (U.S.).; Technical Documentary Report
Responsabilità: E.I. Ergin, V.D. Norum, and T.G. WIndeknecht.

Abstract:

This four volume report was prepared in order to compile, describe, and apply available nonlinear analysis and design techniques for space vehicle attitude control systems and to outline additional areas of future effort to improve present analysis and design procedures. Each of the four volumes is relatively independent of the others. Volume I is a definition and description of the problems associated with the design of the space vehicle attitude control systems. Volume II treats in detail the principal techniques for the analysis of nonlinear control systems and shows the application of these techniques to specific attitude control system problems. Volume III discusses three general problems in space vehicle attitude control systems, (1) single axis on-off gas jet system design, (2) active attitude control system design for a spin-stabilized vehicle, and (3) the design of a control system for a satellite vehicle with reaction wheels and gas jets. Volume IV is a collection of references and bibliography with annotations and comments covering the spectrum of the study effort.

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