BRAKE CONTROL SYSTEM COMPRISING RUNWAY FRICTION PROPERTY ESTIMATION MAPPING
Systems and methods for detecting the onset of wheel skids and controlling brake torque to achieve efficient and smooth braking performance are described herein. A brake control system may utilize an algorithm, along with substantially real-time measured values to assist with controlling brake torque to achieve efficient and smooth braking performance. A history of wheel speed information, such as wheel speed information associated with one or more landing event, may also be used to iteratively estimate tire/runway friction properties.
1 . A method for determining coefficients of friction along a portion of a runway comprising:
measuring, by a flight control processor, a first gear reference speed for a first landing gear of an aircraft;
measuring, by the flight control processor, a first gear instantaneous speed for the first landing gear of the aircraft;
determining, by the flight control processor, a slip ratio of the first landing gear;
estimating, by the flight control processor, a weight of the aircraft associated with the first landing gear;
mapping, by the flight control processor, position data to the measured values; and
estimating, by the flight control processor, coefficients of friction associated with locations along the portion of the runway.
2 . The method of claim 1 , wherein the calculating the first gear reference speed comprises measuring a wheel speed of a wheel on the first landing gear.
3 . The method of claim 1 , wherein the estimating the weight of the aircraft comprises determining a tire pressure of a tire of the first landing gear, and calculating the weight of the aircraft based on the determined change tire pressure from a known reference value.
4 . The method of claim 1 , further comprising transmitting the first gear reference speed from a wheel speed sensor to the flight control processor.
5 . The method of claim 1 , further comprising calculating position data from a location sensor.
6 . The method of claim 5 , wherein the location sensor is a global positioning unit.
7 . The method of claim 1 , wherein the calculating the first gear reference speed comprises averaging a wheel reference speed of a plurality of wheels on the first landing gear.
8 . The method of claim 1 , further comprising determining that lift on wings of the aircraft is not affecting the weight of the aircraft determination.
9 . The method of claim 1 , further comprising transmitting the determined coefficient of friction associated with the portion of the runway to a central processor.
10 . The method of claim 1 , further comprising aggregating determined coefficient of friction information from additional aircraft to establish an expanded mapping of the coefficient of friction associated with the runway.
11 . The method of claim 1 , wherein the portion of the runway is associated with a path of travel of the aircraft.
12 . The method of claim 1 , wherein a lower bound of wheel slip values may be calculated in response to a braking stop comprising no anti-skid system event.
13 . The method of claim 1 , wherein an anti-skid system event associated with the aircraft is used to plot peak wheel accelerations.
14 . The method of claim 13 , wherein peak wheel accelerations are used to estimate wheel slip values.
15 . The method of claim 1 , wherein the determined coefficient of friction associated with the portion of the runway are exploited to detect an onset of a wheel skid.
16 . The method of claim 1 , wherein the determined coefficients of friction associated with the portion of the runway are exploited to achieve smooth braking performance.
17 . An article of manufacture including a non-transitory, tangible computer readable medium having instructions stored thereon that, in response to execution by a computing device, cause the computer-based system to perform operations comprising:
measuring, by the computing device, a first gear reference speed for a first landing gear of an aircraft;
measuring, by the computing device, a first gear instantaneous speed for the first landing gear of the aircraft;
determining, by the computing device, a slip ratio of the first landing gear;
estimating, by the computing device, a weight of the aircraft associated with the first landing gear;
mapping, by the computing device, position data to the measured values; and
estimating, by the computing device, coefficients of friction associated with locations along a portion of a runway.
18 . The article of manufacture of claim 17 , further comprising transmitting, by the computing device, the determined coefficient of friction associated with the portion of the runway to a central processor.
19 . The article of manufacture of claim 17 , further comprising calculating position data from a location sensor.
20 . A system comprising:
a tangible, non-transitory memory communicating with a processor,
the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations comprising:
measuring, by the processor, a first gear reference speed for a first landing gear of an aircraft;
measuring, by the processor, a first gear instantaneous speed for the first landing gear of the aircraft;
determining, by the processor, a slip ratio of the first landing gear;
estimating, by the processor, a weight of the aircraft associated with the first landing gear;
mapping, by the processor, position data to the measured values; and
estimating, by the processor, coefficients of friction associated with locations along a portion of a runway.