9786207459018 - robust linear controller design for attitude control of a rocket di r, sumathi (9 risultati)
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Taschenbuch. Condizione: Neu. Robust Linear Controller Design for Attitude Control of a Rocket | Sumathi R | Taschenbuch | Englisch | 2024 | LAP LAMBERT Academic Publishing | EAN 9786207459018 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot…]de | Anbieter: preigu.
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PAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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PAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, , GermaniaBuchWeltWeit Ludwig Meier e.K.
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 168 pp. Englisch.
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Da: moluna, Greven, , Germaniamoluna
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Attitude control of the rocket is a big challenge in real-time. To make the rocket stable against the influences, this book has examined the control technology such as proportional integral derivative control using a…n anti-windup mechanism and linear quadra.
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000
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Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Attitude control of the rocket is a big challenge in real-time. To make the rocket stable against the influences, this book has examined the control technology such as proportional integral derivative control using an anti-windup mecha…nism and linear quadratic regulator theory based on the degree of freedom mathematical model. The transient behaviour of both controllers is not smooth and takes more time to settle in the defined location. Specific to the deficiencies of PID and LQR, the proportional integral derivative controller is combined with a fuzzy logic controller to overcome the defects of PID and LQR. In conclusion, this book compares the performance analysis of fuzzy-PID controllers with linear quadratic regulators and proportional integral derivative controllers. The simulation results indicate that the hybrid fuzzy-PID controller has a remarkable improvement in terms of overshoot and settling time besides reducing steady-state error. The proposed hybrid fuzzy-PID controller eliminates the overshoot completely and produces enormous stability for the rocket engine.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 168 pp. Englisch.
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Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH
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Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Attitude control of the rocket is a big challenge in real-time. To make the rocket stable against the influences, this book has examined the control technology such as proportional integral derivative control using an anti-windup mechan…ism and linear quadratic regulator theory based on the degree of freedom mathematical model. The transient behaviour of both controllers is not smooth and takes more time to settle in the defined location. Specific to the deficiencies of PID and LQR, the proportional integral derivative controller is combined with a fuzzy logic controller to overcome the defects of PID and LQR. In conclusion, this book compares the performance analysis of fuzzy-PID controllers with linear quadratic regulators and proportional integral derivative controllers. The simulation results indicate that the hybrid fuzzy-PID controller has a remarkable improvement in terms of overshoot and settling time besides reducing steady-state error. The proposed hybrid fuzzy-PID controller eliminates the overshoot completely and produces enormous stability for the rocket engine.
