BRAKING PROCESS FOR AN AIRPLANE
An aircraft braking adaptation process is used to prevent rapid derotation of an aircraft causing damage to the front landing gear by formulating a braking command, applying the command to at least one brake, adapting the braking command by acquiring the aircraft trim and modifying the braking commands as a function of the aircraft trim. This process limits the derotation speed and preserves the front landing gear.
1 . An aircraft braking process that is controlled by an aircraft command logic comprising:
formulating a braking command K,
applying the command to at least one means of braking,
wherein the process is controlled by the aircraft command logic and includes modifying the braking command K, by:
acquiring the aircraft trim A, counted positively to nose up,
modifying the braking command based on the aircraft trim A into a braking command K′.
2 . The process in claim 1 , further comprising that the braking command is modified only if the difference between the trim A and a minimum trim Amin is greater than a predetermined threshold difference ΔSt.
3 . The process in claim 1 , further comprising that the modification of the braking command is eliminated if the braking exceeds a predetermined period of time.
4 . The process in claim 3 , further comprising that the elimination is done degressively over a predetermined period of time.
5 . The process in claim 4 , further comprising that the elimination is linear over time.
6 . The process in claim 1 , further comprising that the adaptation of the braking command continuously combines, at each possible value A of trim, a weighted coefficient P(A) of an initial braking command, and the modified command is then the product of the initial command times the weighted coefficient.
7 . The process in claim 6 , further comprising that P(A) has a value of “one” if the difference between the trim A and a minimum trim Amin is less than or equal to a strictly positive threshold difference ΔSt, and P(A) has a constant value strictly less than on in the other cases.
8 . The process in claim 6 , further comprising that P(A) has the value “one” if the difference between the trim A and a minimum trim Amin is less than or equal to a positive threshold difference ΔSt or zero, and P(A) is a decreasing function of A from a value of 1.
9 . The process in claim 8 , further comprising that the decrease is linear.
10 . The process in claim 8 , further comprising that the decrease is hyperbolic.