Singh, Rithesh and Rao, Vidya S (2011) Modeling and Simulation of Antiskid Brake System for Fighter Aircrafts. In: CISCON – 2010, 2011, Manipal Institute of Technology, Manipal..
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Abstract
Aircraft brake system plays a very important role in the safe takeoff and landing. On landing, skid phenomena is observed due to runway surfaces, pilot brake demand or due to other factors which creates unsafe for the aircraft while landing. So we use anti-skid braking system which will prevent tires from slipping extremely on the track and ensure aircraft landing safety and stability with maximum braking efficiency. This paper presents modeling and simulation part of the work for the aircraft brake system.
Item Type: | Conference or Workshop Item (Paper) |
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Uncontrolled Keywords: | μ-slip curve, slip ratio, wheel speed transducer, brake discs, hydraulic system, anti-skid |
Subjects: | Engineering > MIT Manipal > Instrumentation and Control |
Depositing User: | MIT Library |
Date Deposited: | 22 Oct 2016 15:46 |
Last Modified: | 22 Oct 2016 15:46 |
URI: | http://eprints.manipal.edu/id/eprint/147371 |
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