Automatic reverse idle arming uses landing-condition detection to trigger thrust reversers faster and reduce runway excursion risk.
Automatic touchdown detection triggers thrust reversers from reverse idle, cutting pilot reaction delay and braking distance on wet or short runways.
Conservative runway assumptions can distort landing indicators; this case uses runway and retardation data to improve distance estimates.
A brake system determines stack closure pressure using pressure transducers and a control valve to modulate fluid flow.
A brake de-selection controller calculates energy input from torque and wheel speed to selectively disable brakes.
Replacing mechanical interlocks with a digital graphical interface frees instrument panel space while reducing aircraft weight and maintenance complexity.
Automated processing circuit reduces pilot decision time by 2-4 seconds, preventing runway overrun accidents after engine failures.
Electro-hydraulic valves enable remote emergency park braking while reducing system weight through segmented power sources.
Electronic sensors replace qualitative verbal reports with quantitative braking data, eliminating traffic halts while providing accurate traction estimates.
A predictive braking method estimates taxiing brake temperatures to optimize path selection and reduce component wear.
An aircraft control module calculates deceleration distances for brake and thrust reverser configurations to identify the lowest total cost equipment setting.
Automated control module adjusts nose gear steering angle and braking force to prevent loss of adhesion during ground operations.
Automated control system manages aircraft taxi speed using real-time engine thrust adjustments to eliminate jerky deceleration and reduce brake wear.
Autobraking system maintains aircraft course stability by applying differential braking forces based on yaw error feedback.
Dynamic braking control reduces runway occupancy time and thermal energy generation by optimizing deceleration profiles against exit targets.