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Techniques for analysis of nonlinear attitude control systems for space vehicles. Vol. 3. Examples of analytical design of space craft attitude control systems

著者: E I ErginV D NorumT G WindeknechtUnited States. Air Force. Systems Command. Aeronautical Systems Division.Space Technology Laboratories, inc.所有著者
出版商: Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962.
丛书: Technical documentary report (United States. Air Force. Systems Command. Aeronautical Systems Division), ASD TDR 62-208/v.3.
版本/格式:   打印图书 : 国家级的政府刊物 : 英语
提要:
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  再读一些...
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材料类型: 政府刊物, 国家级的政府刊物
文档类型 图书
所有的著者/提供者: 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号码: 444661048
注释: "June 1962."
"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.
描述: vi, 70 pages ; 28 cm.
丛书名: Technical documentary report (United States. Air Force. Systems Command. Aeronautical Systems Division), ASD TDR 62-208/v.3.
其他题名: Examples of analytical design of space craft attitude control systems
责任: 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

摘要:

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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