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
100 pages
Report
Keine Angabe
Englisch
Dynamics of aircraft antiskid braking systems
NTRS | 1982
|Intelligent Aircraft Antiskid Braking Systems – A Review
Springer Verlag | 2024
|