A computer study was performed to assess the accuracy of three brake pressure-torque mathematical models. The investigation utilized one main gear wheel, brake, and tire assembly of a McDonnell Douglas DC-9 series 10 airplane. The investigation indicates that the performance of aircraft antiskid braking systems is strongly influenced by tire characteristics, dynamic response of the antiskid control valve, and pressure-torque response of the brake. The computer study employed an average torque error criterion to assess the accuracy of the models. The results indicate that a variable nonlinear spring with hysteresis memory function models the pressure-torque response of the brake more accurately than currently used models.
Dynamics of aircraft antiskid braking systems
1982-02-01
Report
No indication
English
Dynamics of Aircraft Antiskid Braking Systems
NTIS | 1982
|Intelligent Aircraft Antiskid Braking Systems – A Review
Springer Verlag | 2024
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