Additional safety feature in aircraft braking system
A method for braking an aircraft is disclosed herein. The method includes receiving, by a brake controller, a first signal from a position sensor of a first pedal, receiving, by the brake controller, a second signal from a pedal sensor of the first pedal, determining, by the brake controller, that the pedal is being pressed based on the first and second signals, and sending, by the brake controller, an instruction to apply a brake pressure in response to the determination that the pedal is being pressed.
1. A method of braking an aircraft, comprising:
receiving, by a brake controller, a first signal from a position sensor of a first pedal;
receiving, by the brake controller, a second signal from a pedal sensor of the first pedal;
determining, by the brake controller, that the pedal is being pressed based on the first and second signals;
calculating, by the brake controller, an amount of pressure to apply based on the first signal;
receiving, by the brake controller, a second amount of pressure to apply from a second brake controller;
comparing, by the brake controller, the amount of pressure to apply and the second amount of pressure to apply; and
sending, by the brake controller, an instruction to apply a brake pressure in response to the determination that the amount of pressure and the second amount of pressure are the same.
2. The method of claim 1 , wherein the instruction to apply the brake pressure is based at least in part on the first signal.
3. The method of claim 1 , further comprising:
receiving, by the brake controller, a third signal from a second position sensor of a second pedal;
receiving, by the brake controller, a fourth signal from a second pedal sensor of the second pedal;
determining, by the brake controller, that the second pedal is being pressed further than the first pedal based on the third and fourth signals; and
sending, by the brake controller, the instruction to apply the brake pressure based on the third signal.
4. The method of claim 1 , further comprising:
detecting, by the brake controller, a fault based at least in part on the first signal and the second signal prior to sending the instruction to apply the brake pressure.
5. The method of claim 1 , wherein the position sensor provides an indication of how much the first pedal is displaced.
6. The method of claim 1 , wherein the pedal sensor provides an indication of whether or not the first pedal is being pressed.
7. An article of manufacture including a tangible, non-transitory computer-readable storage medium having instructions stored thereon that, in response to execution by a processor, cause the processor to perform operations comprising:
receiving, by a brake controller, a first signal from a position sensor of a pedal;
receiving, by the brake controller, a second signal from a pedal sensor of the pedal;
determining, by the brake controller, whether or not the pedal is being pressed based on the first signal and the second signal;
calculating, by the brake controller, an amount of pressure to apply based on the first signal;
receiving, by the brake controller, a second amount of pressure to apply from a second brake controller;
comparing, by the brake controller, the amount of pressure to apply and the second amount of pressure to apply; and
sending, by the brake controller, an instruction to apply a brake pressure in response to a determination that the amount of pressure and the second amount of pressure are the same.
8. The article of manufacture of claim 7 , wherein the position sensor provides an indication of how far the pedal has travelled.
9. The article of manufacture of claim 7 , wherein the pedal sensor provides an indication of whether or not the pedal is being pressed.
10. The article of manufacture of claim 7 , wherein the operations further comprise:
identifying, by the brake controller, a fault based at least in part on the first signal and the second signal.
11. The article of manufacture of claim 7 , wherein the operations further comprise:
receiving, by the brake controller, a third signal from a second position sensor of a second pedal;
comparing, by the brake controller, the first signal and the third signal; and
sending, by the brake controller, the instructions to apply the brake pressure based on the first signal, the first signal being greater than the third signal.
12. A brake system for an aircraft, comprising:
a brake assembly configured to supply a brake pressure in response to a pedal being displaced;
a position sensor configured to provide an indication of an amount of displacement of the pedal;
a pedal sensor configured to provide an indication that the pedal is being displaced; and
a brake controller configured to control the brake pressure, the brake controller configured to:
receive a first signal from the position sensor;
receive a second signal from the pedal sensor;
determine that the pedal is being activated;
calculate an amount of pressure to apply based on the first signal;
receive a second amount of pressure to apply from a second brake controller;
compare the amount of pressure to apply and the second amount of pressure to identify a fault in the brake system based on the comparison; and
modify the brake pressure as a function of pedal displacement in response to the identification of a fault.
13. The brake system of claim 12 , wherein the determination that the pedal is being activated is based on the first signal.
14. The brake system of claim 13 , wherein the determination that the pedal is being activated is further based on the second signal.
15. The brake system of claim 12 , wherein the pedal sensor provides an indication that the pedal is being pressed.