A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis

Document Number: 2002-01-2949

Date Published: November 2002

Author(s):
James R. Phillips - Honeywell Aircraft Landing Systems

Abstract:
A dynamical model of tire longitudinal slip, suitable for use in aircraft brake control system and antiskid design, is presented. The model differs from conventional mu-slip models in that it incorporates a single degree of freedom for tire stretch. Applications of the model in simulation, control synthesis, and stability analyses are described.

File Size: 191K
Product Status: In Stock

See other papers presented at World Aviation Congress _® & Display, November 2002, Phoenix, AZ, USA, Session: Aircraft System / Braking

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