Systems and methods for pressure control mixed mode for braking operation
A brake control system of the present disclosure calibrates a servo valve and calculates a calibrated transfer function associated with the servo valve for precise braking in open-loop mode. The calibration steps may include determining i) whether an aircraft is on a ground surface, ii) whether the aircraft is not moving relative to the ground surface, and iii) whether braking is applied to a brake system of the aircraft. The brake control unit may calibrate the servo valve in response to the brake control unit determining that i) the aircraft is on the ground surface, ii) the aircraft is not moving relative to the ground surface, and iii) the braking is not applied to the brake system of the aircraft. The calibration process includes sending two or more test currents to the servo valve, and determining braking pressures associated with those test currents to calculate the transfer function.
1. A brake control system, comprising:
a servo valve configured to receive a hydraulic fluid and provide the hydraulic fluid to apply a braking force to a wheel via a hydraulic line; and
a brake control unit in electronic communication with the servo valve;
wherein the brake control unit is configured to:
determine whether an aircraft is on a ground surface and not moving relative to the ground surface;
determine whether braking is applied to a brake system of the aircraft; and
calibrate the servo valve in response to the brake control unit determining that i) the aircraft is on the ground surface, ii) the aircraft is not moving relative to the ground surface, and iii) the braking is not applied to the brake system of the aircraft;
the brake control unit calibrates the servo valve by a method comprising:
sending a first electric current to the servo valve;
in response to the first electric current being sent to the servo valve, determining, with a pressure sensor, a first pressure applied to the brake system via the servo valve;
sending a second electric current to the servo valve; and
in response to the second electric current being sent to the servo valve, determining with the pressure sensor a second pressure applied to the brake system via the servo valve.
2. The brake control system of claim 1 , wherein the calibrating further comprises calculating, by the brake control unit, a braking pressure versus servo valve current curve based upon the first electric current, the first pressure, the second electric current, and the second pressure.
3. The brake control system of claim 1 , wherein the calibrating further comprises calculating, by the brake control unit, a transfer function associated with the servo valve using the first electric current, the first pressure, the second electric current, and the second pressure.
4. The brake control system of claim 1 , wherein the second electric current is sent to the servo valve for a predetermined duration, and the second pressure is an average pressure measured during the predetermined duration.
5. The brake control system of claim 1 , wherein the brake control unit is further configured to:
determine whether the calibration of the servo valve was successful;
operate as an open-loop system in response to the calibration being successful; and
operate as a closed-loop system in response to the calibration being unsuccessful.
6. The brake control system of claim 3 , wherein the transfer function is used for calculating an electric current for a desired braking pressure commanded via the servo valve.
7. The brake control system of claim 6 , wherein the brake control unit is further configured to operate the servo valve based on the electric current calculated using the transfer function.
8. The brake control system of claim 1 , wherein:
the calibrating further comprises calculating, by the brake control unit, a transfer function associated with the servo valve using the first electric current, the first pressure, the second electric current, and the second pressure;
the transfer function is used for calculating an electric current for a desired braking pressure commanded via the servo valve; and
the brake control unit is further configured to:
determine whether the calibration of the servo valve was successful;
operate as an open-loop system in response to the calibration being successful, wherein the brake control unit uses the transfer function for calculating a servo valve command current; and
operate as a closed-loop system in response to the calibration being unsuccessful.
9. A method for operating a brake control unit, comprising:
initiating, by the brake control unit, a servo valve calibration process;
determining, by the brake control unit, whether an aircraft is on a ground surface and not moving relative to the ground surface;
determining, by the brake control unit, whether braking is applied to a brake system of the aircraft; and
calibrating, by the brake control unit, a servo valve in response to the brake control unit determining that the aircraft is on the ground surface and not moving relative to the ground surface, and that braking is not applied to the brake system of the aircraft;
the brake control unit calibrates the servo valve by a method comprising:
sending a first electric current to the servo valve;
in response to the first electric current being sent to the servo valve, determining, with a pressure sensor, a first pressure applied to the brake system via the servo valve;
sending a second electric current to the servo valve; and
in response to the second electric current being sent to the servo valve, determining with the pressure sensor a second pressure applied to the brake system via the servo valve.
10. The method of claim 9 , wherein the calibrating further comprises calculating, by the brake control unit, a braking pressure versus servo valve current curve based upon the first electric current, the first pressure, the second electric current, and the second pressure.
11. The method of claim 9 , wherein the calibrating further comprises calculating, by the brake control unit, a transfer function associated with the servo valve using the first electric current, the first pressure, the second electric current, and the second pressure.
12. The method of claim 9 , wherein the second electric current is sent to the servo valve for a predetermined duration, and the second pressure is an average pressure measured during the predetermined duration.
13. The method of claim 9 , further comprising:
determining, by the brake control unit, whether the calibration of the servo valve was successful;
commanding, by the brake control unit, braking in an open-loop fashion in response to the calibration being successful; and
commanding, by the brake control unit, braking in a closed-loop fashion in response to the calibration being unsuccessful.