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

Auteur: E I ErginV D NorumT G WindeknechtUnited States. Air Force. Systems Command. Aeronautical Systems Division.Space Technology Laboratories, inc.Alle auteurs
Uitgever: Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962.
Serie: Technical documentary report (United States. Air Force. Systems Command. Aeronautical Systems Division), ASD TDR 62-208/v.1.
Editie/Formaat:   Gedrukt boek : Nationale overheidsuitgave : Engels
Samenvatting:
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  Meer lezen...
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Details

Genre: Overheidsuitgave, Nationale overheidsuitgave
Soort document Boek
Alle auteurs / medewerkers: E I Ergin; V D Norum; T G Windeknecht; United States. Air Force. Systems Command. Aeronautical Systems Division.; Space Technology Laboratories, inc.; Wright-Patterson Air Force Base (Ohio)
OCLC-nummer: 444644271
Opmerkingen: "June 1962."
AD0282057 (from http://www.dtic.mil).
"Project No. 8219, Task No. 82165." -- cover.
Research supported by the United States Air Force, Air Force Systems Command, and performed by Space Technology Laboratories, Inc.
Beschrijving: viii, 90 pages : illustrations ; 28 cm.
Serietitel: Technical documentary report (United States. Air Force. Systems Command. Aeronautical Systems Division), ASD TDR 62-208/v.1.
Andere titels: Characteristics of the spacecraft attitude control problem
Verantwoordelijkheid: prepared under Contract No. AF 33(616)-7811 by Space Technology Laboratories, Inc, Redondo Beach, California. Authors: E.I. Ergin, V.D. Norum, and T.G. WIndeknecht.

Fragment:

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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