During an aircraft stop, the load may range from nearly nothing at brake application (when many aircraft are still nearly airborne) to greater value than the static loads. The energies absorbed by aircraft brakes are orders of higher magnitude. Aircraft anti-skid brake system uses sensors monitoring the movement of aircraft, and controls the system according to how much the wheel slide. This system can be developed from a number of switching techniques called anti-skid braking system. In this work, slip-ratio-controlled technique is used for the aircraft brake system. During fault-free condition of operation, it shall be able to stop the aircraft in minimum possible distance without any wheel lock condition under various braking conditions like runway type, runway and type characteristics, braking speed, landing load and brake pad characteristics. An estimate of slip is estimated using a technique called H∞ filter design. The purpose of estimation is to make the slip, error free, from the unwanted noises coming out from the sensors and other measuring devices which affect the system parameters.
Mr. Ritesh Singh received his M Tech in Control Systems from Manipal University, Manipal, Karnataka,India in 2012. His area of research includes:Advanced Control Techniques,Flight Control Systems and Model Based Design. He has published research papers in national and international journals and has active participation in workshops and conferences.
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Vendeur : moluna, Greven, Allemagne
Kartoniert / Broschiert. Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Singh RiteshMr. Ritesh Singh received his M Tech in Control Systems from Manipal University, Manipal, Karnataka,India in 2012. His area of research includes:Advanced Control Techniques,Flight Control Systems and Model Based Design. H. N° de réf. du vendeur 5142099
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Vendeur : Revaluation Books, Exeter, Royaume-Uni
Paperback. Etat : Brand New. 60 pages. 8.66x5.91x0.14 inches. In Stock. N° de réf. du vendeur 3659238074
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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - During an aircraft stop, the load may range from nearly nothing at brake application (when many aircraft are still nearly airborne) to greater value than the static loads. The energies absorbed by aircraft brakes are orders of higher magnitude. Aircraft anti- skid brake system uses sensors monitoring the movement of aircraft, and controls the system according to how much the wheel slide. This system can be developed from a number of switching techniques called anti- skid braking system. In this work, slip-ratio-controlled technique is used for the aircraft brake system. During fault-free condition of operation, it shall be able to stop the aircraft in minimum possible distance without any wheel lock condition under various braking conditions like runway type, runway and type characteristics, braking speed, landing load and brake pad characteristics. An estimate of slip is estimated using a technique called H filter design. The purpose of estimation is to make the slip, error free, from the unwanted noises coming out from the sensors and other measuring devices which affect the system parameters. N° de réf. du vendeur 9783659238079
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Vendeur : preigu, Osnabrück, Allemagne
Taschenbuch. Etat : Neu. H Filter Design | Anti-skid Braking System for Fighter Aircrafts | Ritesh Singh | Taschenbuch | Englisch | LAP Lambert Academic Publishing | EAN 9783659238079 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 106221870
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