컨텐츠로 이동
Techniques for analysis of nonlinear attitude control systems. Vol. 2. Techniques for analysis and synthesis of nonlinear control systems 해당 항목을 미리보기
닫기해당 항목을 미리보기
확인중입니다…

Techniques for analysis of nonlinear attitude control systems. Vol. 2. Techniques for analysis and synthesis of nonlinear control systems

저자: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.).; Space Technology Laboratories, Inc.
출판사: Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962.
시리즈: Aeronautical Systems Division (U.S.).; Technical Documentary Report
판/형식:   도서 : 국가 정부 간행물 : 영어
데이터베이스:WorldCat
요약:
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  더 읽기…
평가:

(아무런 평가가 없습니다.) 0 리뷰와 함께 - 첫번째로 올려주세요.

주제
다음과 같습니다:

 

도서관에서 사본 찾기

&AllPage.SpinnerRetrieving; 해당항목을 보유하고 있는 도서관을 찾는 중

상세정보

자료 유형: 정부 간행물, 국가 정부 간행물
문서 형식:
모든 저자 / 참여자: E I Ergin; V D Norum; T G Windeknecht; Aeronautical Systems Division (U.S.).; Space Technology Laboratories, Inc.
OCLC 번호: 444602829
메모: "June 1962."
AD0282805 (from http://www.dtic.mil).
Research supported by the United States Air Force, Air Force Systems Command, and performed by Space Technology Laboratories, Inc.
설명: xii, 302 p. : ill. ; 28 cm.
일련 제목: Aeronautical Systems Division (U.S.).; Technical Documentary Report
책임: E. I. Ergin, V. D. Norum, and T. G. WIndeknecht.

초록:

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.

리뷰

사용자-기여 리뷰
GoodReads 리뷰 가져오는 중…
DOGObooks 리뷰를 가지고 오는 중…

태그

첫번째 되기
요청하신 것을 확인하기

이 항목을 이미 요청하셨을 수도 있습니다. 만약 이 요청을 계속해서 진행하시려면 Ok을 선택하세요.

링크된 데이터


<http://www.worldcat.org/oclc/444602829>
library:oclcnum"444602829"
library:placeOfPublication
library:placeOfPublication
rdf:typeschema:Place
schema:name"Wright-Patterson Air Force Base, Ohio"
owl:sameAs<info:oclcnum/444602829>
rdf:typeschema:Book
rdfs:seeAlso
schema:about
schema:about
schema:about
schema:about
schema:about
schema:about
<http://id.worldcat.org/fast/817353>
rdf:typeschema:Intangible
schema:name"Artificial satellites--Attitude control systems"
schema:about
schema:about
schema:author
schema:contributor
rdf:typeschema:Organization
schema:name"Aeronautical Systems Division (U.S.)."
schema:contributor
schema:contributor
schema:contributor
schema:datePublished"1962"
schema:description"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."
schema:exampleOfWork<http://worldcat.org/entity/work/id/1810492294>
schema:inLanguage"en"
schema:name"Techniques for analysis of nonlinear attitude control systems. Vol. 2. Techniques for analysis and synthesis of nonlinear control systems"
schema:numberOfPages"302"
schema:publisher
rdf:typeschema:Organization
schema:name"Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force"

Content-negotiable representations

윈도우 닫기

WorldCat에 로그인 하십시오 

계정이 없으세요? 아주 간단한 절차를 통하여 무료 계정을 만드실 수 있습니다.