Fuzzy logic antiskid control system for aircraft

Details Fuzzy logic antiskid control system for aircraft Fuzzy logic antiskid control system for aircraft

1996-10-25

2000-07-11

Cuchlinski, Jr., William A.

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Indication or control of braking, acceleration, or deceleration

244111, 303126, B60T 712, G06F 1700

Patent

active

060886463

ABSTRACT:
An antiskid control system for aircraft braking consisting of an iterative system having inputs including wheel speed, time since touchdown and the value of the control current generated by the previous iteration. Utilizing the previous value and applying fuzzy logic rules, the system modifies itself to adjust for variations in the coefficient of friction between the wheels and the runway.

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