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About this product
Product Identifiers
PublisherPrinceton University Press
ISBN-100691087822
ISBN-139780691087825
eBay Product ID (ePID)102900248
Product Key Features
Number of Pages408 Pages
Publication NameControl of Spacecraft and Aircraft
LanguageEnglish
Publication Year1994
SubjectAeronautics & Astronautics
TypeTextbook
Subject AreaTechnology & Engineering
AuthorArthur E. Bryson Jr., Arthur E. Bryson
FormatHardcover
Dimensions
Item Height1.2 in
Item Weight17 Oz
Item Length9.5 in
Item Width6.4 in
Additional Product Features
Intended AudienceCollege Audience
LCCN92-029102
Dewey Edition20
Reviews"The text reads very smoothly, and I found it very well edited. . . . I very much enjoyed reading it and find it a welcome addition to the available dynamics and control texts." -- American Scientist, The text reads very smoothly, and I found it very well edited. . . . I very much enjoyed reading it and find it a welcome addition to the available dynamics and control texts., "The text reads very smoothly, and I found it very well edited. . . . I very much enjoyed reading it and find it a welcome addition to the available dynamics and control texts."-- American Scientist, The text reads very smoothly, and I found it very well edited. . . . I very much enjoyed reading it and find it a welcome addition to the available dynamics and control texts. -- American Scientist
IllustratedYes
Dewey Decimal629.1326
SynopsisProvides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. This book describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot., Here a leading researcher provides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. In this book Arthur Bryson describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot. The first half of the work is about attitude control of rigid and flexible spacecraft using momentum wheels, spin, fixed thrusters, and gimbaled engines. Guidance for nearly circular orbits is discussed. The second half is about aircraft attitude and flight path control. This section discusses autopilot designs for cruise, climb-descent, coordinated turns, and automatic landing. One chapter deals with controlling helicopters near hover, and another offers an introduction to the stabilization of aeroelastic instabilities. Throughout the book there is a strong emphasis on the mathematical modeling necessary for designing a good feedback control system. The appendixes summarize analysis of linear dynamic systems, synthesis of analog and digital feedback control, simulation, and modeling of flexible vehicles.