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.Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
Arthur E. Bryson, Jr., is Paul Pigott Professor of Engineering at Stanford University. Coauthor, with Y. C. Ho, of Applied Optimal Control (Blaisdell/ Hemisphere), he is a member of the National Academy of Engineering and the National Academy of Sciences.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
Vendeur : World of Books (was SecondSale), Montgomery, IL, Etats-Unis
Hardback. Etat : Good. 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. N° de réf. du vendeur 00110446126
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Vendeur : World of Books Inc, Montgomery, IL, Etats-Unis
Hardback. Etat : Good. 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. N° de réf. du vendeur CIN0691087822G
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Vendeur : Goodwill of Central and Coastal Virginia, Richmond, VA, Etats-Unis
Etat : acceptable. N° de réf. du vendeur CCVV.0691087822.A
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Vendeur : Hamelyn, Madrid, M, Espagne
Etat : Very Good. : Este libro ofrece un tratamiento exhaustivo sobre el diseño de lógica de control automático para naves espaciales y aeronaves. El autor, Arthur E. Bryson, describe el método del regulador lineal-cuadrático (LQR) para la síntesis de control por retroalimentación, permitiendo coordinar múltiples controles y lograr maniobras precisas comparables a las de un piloto experto.La primera parte de la obra se centra en el control de actitud de naves espaciales rígidas y flexibles, abordando el uso de volantes de inercia, propulsores y motores articulados. La segunda parte se dedica al control de actitud y trayectoria de vuelo de aeronaves, incluyendo diseños de piloto automático para diversas fases de vuelo, control de helicópteros y estabilización de inestabilidades aeroelásticas, con un fuerte énfasis en el modelado matemático necesario para sistemas de control eficaces. EAN: 9780691087825 Tipo: Libros Categoría: Tecnología Título: Control of Spacecraft and Aircraft Autor: Arthur E. Bryson Editorial: Princeton University Press Idioma: en Páginas: 408 Formato: tapa dura. N° de réf. du vendeur Happ-2026-08-03-9a8e4a26
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Vendeur : Labyrinth Books, Princeton, NJ, Etats-Unis
Etat : New. N° de réf. du vendeur 131918
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Vendeur : Antiquariat Bernhardt, Kassel, Allemagne
Etat : Sehr gut. Mit Abbildungen, XXIII, 378 S. Zust: Gutes Exemplar. Schneller Versand und persönlicher Service - jedes Buch händisch geprüft und beschrieben - aus unserem Familienbetrieb seit über 25 Jahren. Eine Rechnung mit ausgewiesener Mehrwertsteuer liegt jeder unserer Lieferungen bei. Wir versenden mit der deutschen Post. Sprache: Englisch Gewicht in Gramm: 746 gebundene Ausgabe gebundene Ausgabe. N° de réf. du vendeur 487132
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Vendeur : GreatBookPrices, Columbia, MD, Etats-Unis
Etat : New. N° de réf. du vendeur 400382-n
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Vendeur : PBShop.store US, Wood Dale, IL, Etats-Unis
HRD. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur WP-9780691087825
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Vendeur : PBShop.store UK, Fairford, GLOS, Royaume-Uni
HRD. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur WP-9780691087825
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Vendeur : Buchpark, Trebbin, Allemagne
Etat : Sehr gut. Zustand: Sehr gut | Seiten: 406 | Sprache: Englisch | Produktart: Bücher | 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. N° de réf. du vendeur 2652605/202
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