Informazioni su questo prodotto

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.