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

著者: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.); Space Technology Laboratories, inc.
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: Aeronautical Systems Division (U.S.).; Technical Documentary Report
版本/格式:   Print book : 国家级的政府刊物 : 英语
数据库:WorldCat
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
文件类型:
所有的著者/提供者: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.); Space Technology Laboratories, inc.
OCLC号码: 444644271
注意: "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.
描述: viii, 90 pages : illustrations ; 28 cm.
丛书名: Aeronautical Systems Division (U.S.).; Technical Documentary Report
责任: 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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