Kniha H  Filter Design Ritesh Singh

H Filter Design

Anti-skid Braking System for Fighter Aircrafts

Autor: Ritesh Singh
Jazyk: Angličtina
Vazba: Brožovaná
Dostupnost: U nakladatele na objednávku
Odesíláme za 17-27 dnů
1 173
During an aircraft stop, the load may range from nearly nothing at brake application (when many airc...

Informace o knize

Autor
Jazyk
Angličtina
Vazba
Kniha - Brožovaná
Vydáno
2012
Stránek
60
EAN
9783659238079
Enbook ID
07091610
Hmotnost
106
Rozměry
150 x 220 x 4

Kompletní popis

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.

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