H∞ Filter Design: Anti-skid Braking System for Fighter Aircrafts - Softcover

Singh, Ritesh

 
9783659238079: H∞ Filter Design: Anti-skid Braking System for Fighter Aircrafts
Softcover
ISBN 10: 3659238074 ISBN 13: 9783659238079
Verlag: LAP LAMBERT Academic Publishing, 2012

Reseña del editor

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.

Biografía del autor

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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Verlag
LAP LAMBERT Academic Publishing
Erscheinungsdatum
2012
Sprache
Englisch
ISBN 10 
3659238074
ISBN 13 
9783659238079
Einband
Tapa blanda
Anzahl der Seiten
60
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