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A Sliding Mode Observer Based ABS for Aircraft and Land Vehicles
Technical Paper
2003-01-0252
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
Control of an antilock brake system for aircraft and land vehicles is based upon estimates of the torque applied to braking wheels by means of a sliding mode observer. The observer yields a highly accurate estimate of torque that is robust for the entire operating range of the brakes, and provides an input to a relatively simple control system that regulates applied torque from either an electro-hydraulic or electromechanical actuator. Excellent braking performance for a regional jet transport is demonstrated in this paper via hardware-in-the-loop simulation. A simple scheme for suppressing gear walk (aircraft application) is presented.
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Authors
Citation
Ribbens, W. and Fredricks, R., "A Sliding Mode Observer Based ABS for Aircraft and Land Vehicles," SAE Technical Paper 2003-01-0252, 2003, https://doi.org/10.4271/2003-01-0252.Also In
SAE 2003 Transactions Journal of Passenger Cars - Mechanical Systems
Number: V112-6; Published: 2004-09-15
Number: V112-6; Published: 2004-09-15
References
- Kade A. Antilock Brake Control System US Patent No. 4, 673, 225 January 16 1987
- Rudd R. E. Antiskid Brake Control System Using Kalman Filtering US Patent No. 5, 918, 951 July 6 1999
- Unsal Kachroo Sliding Mode Measurement Feedback Control for Antilock Braking System IEEE Trans on Control Theory March 1999 7 271 281
- Drakonov S. Sliding Mode Observer Based on Equivalent Control Methods 31st CDC Conference Tucson AZ Dec. 1992 2368 2370
- Enright J. J. Laboratory Simulation of Landing Gear Pitch-Plane Dynamics SAE paper 851937 Aerospace Technology Conference and Exposition Long Beach, CA October 1985