Aircraft tail strike detection and prevention system and method
One example of an aircraft tail strike detection and prevention system can include one or more processors that obtain one or more aircraft characteristics representative of an aircraft flying toward a landing location and one or more external characteristics representative of one or more conditions outside of the aircraft. The one or more processors can obtain a current descent trajectory that the aircraft is to follow to land at the landing location and calculate a probability that the aircraft will experience a tail strike upon touchdown based on the one or more aircraft characteristics and the one or more external characteristics. The one or more processors can alert a pilot of the aircraft that the aircraft will experience the tail strike upon touchdown based on the probability.
1 . An aircraft tail strike detection and prevention system comprising:
one or more processors configured to obtain one or more aircraft characteristics representative of an aircraft flying toward a landing location and one or more external characteristics representative of one or more conditions outside of the aircraft,
the one or more processors configured to obtain a current descent trajectory that the aircraft is to follow to land at the landing location and calculate a probability that the aircraft will experience a tail strike upon touchdown based on the one or more aircraft characteristics and the one or more external characteristics,
the one or more processors configured to alert a pilot of the aircraft that the aircraft will experience the tail strike upon touchdown based on the probability, and the one or more processors configured to instruct the pilot to follow one or more of a speed adjustment, a provisional flight plan, a go-around procedure, and a missed approach procedure calculated responsive to the probability.
2 . The aircraft tail strike detection and prevention system of claim 1 , wherein the one or more processors are configured to calculate a calculated descent trajectory that differs from the current descent trajectory and that reduces or eliminates the probability that the aircraft will experience the tail strike upon touchdown.
3 . The aircraft tail strike detection and prevention system of claim 2 , wherein the one or more processors are configured to calculate the calculated descent trajectory by changing one or more flare angles of the aircraft from the current descent trajectory at one or more different locations during descent of the aircraft toward the landing location.
4 . The aircraft tail strike detection and prevention system of claim 2 , wherein the one or more processors are configured to automatically control the aircraft during descent to the landing location according to the calculated descent trajectory.
5 . The aircraft tail strike detection and prevention system of claim 2 , wherein the one or more processors are configured to calculate the go-around procedure for the aircraft to circle back and make another attempt at landing at the landing location responsive to the probability of the calculated descent trajectory resulting in the tail strike being larger than a threshold probability.
6 . The aircraft tail strike detection and prevention system of claim 2 , wherein the one or more processors are configured to calculate the calculated descent trajectory based on one or more of an altitude of the aircraft, a vertical approach speed of the aircraft, a pitch rate of the aircraft, a pitch attitude of the aircraft, an engine thrust of the aircraft, a flight path angle of the aircraft, a stall speed of the aircraft, an angle of attack of the aircraft, a sink rate of the aircraft, a glide slope of the aircraft, a landing weight of the aircraft, or a flare angle of the aircraft.
7 . The aircraft tail strike detection and prevention system of claim 1 , wherein the one or more aircraft characteristics include one or more of aircraft gross weight, a landing weight, an amount or weight of fuel onboard the aircraft, a pitch angle or flare angle of the aircraft, or positions of flaps of the aircraft.
8 . The aircraft tail strike detection and prevention system of claim 1 , wherein the one or more external characteristics include one or more of a weather condition or a runway condition.
9 . The aircraft tail strike detection and prevention system of claim 1 , wherein the one or more processors are configured to obtain the one or more aircraft characteristics and the one or more external characteristics, obtain the current descent trajectory, calculate the probability that the aircraft will experience the tail strike upon touchdown, and alert the pilot of the aircraft that the aircraft will experience the tail strike upon touchdown prior to the aircraft reaching an initial approach fix of landing of the aircraft.
10 . An aircraft tail strike prevention method comprising:
obtaining one or more aircraft characteristics representative of an aircraft flying toward a landing location;
obtaining one or more external characteristics representative of one or more conditions outside of the aircraft;
obtaining a current descent trajectory that the aircraft is to follow to land at the landing location;
calculating a probability that the aircraft will experience a tail strike upon touchdown based on the one or more aircraft characteristics and the one or more external characteristics;
alerting a pilot of the aircraft that the aircraft will experience the tail strike upon touchdown based on the probability; and
instructing the pilot to follow one or more of a speed adjustment, provisional flight plan, a go-around procedure, and a missed approach procedure calculated responsive to the probability.
11 . The aircraft tail strike prevention method of claim 10 , further comprising:
calculating a calculated descent trajectory that differs from the current descent trajectory and that reduces or eliminates the probability that the aircraft will experience the tail strike upon touchdown.
12 . The aircraft tail strike prevention method of claim 11 , wherein the calculated descent trajectory is calculated by changing one or more flare angles of the aircraft from the current descent trajectory at one or more different locations during descent of the aircraft toward the landing location.
13 . The aircraft tail strike prevention method of claim 11 , further comprising:
automatically controlling the aircraft during descent to the landing location according to the calculated descent trajectory.
14 . The aircraft tail strike prevention method of claim 11 , further comprising:
calculating the go-around procedure for the aircraft to circle back and make another attempt at landing at the landing location responsive to the probability of the calculated descent trajectory resulting in the tail strike being larger than a threshold probability.
15 . The aircraft tail strike prevention method of claim 11 , wherein the calculated descent trajectory is calculated based on one or more of an altitude of the aircraft, a vertical approach speed of the aircraft, a pitch rate of the aircraft, a pitch attitude of the aircraft, an engine thrust of the aircraft, a flight path angle of the aircraft, a stall speed of the aircraft, an angle of attack of the aircraft, a sink rate of the aircraft, a glide slope of the aircraft, a landing weight of the aircraft, or a flare angle of the aircraft.
16 . An aircraft tail strike detection and prevention system comprising:
a control unit configured to calculate a probability that a tail strike will occur upon touchdown during landing of an aircraft based on one or more aircraft characteristics representative of the aircraft and one or more external characteristics representative of one or more conditions outside of the aircraft;
one or more databases storing one or more of navigation data, obstacle data, engine data, or terrain data; and
an output device configured to present an alert to a pilot of the aircraft,
the control unit configured to calculate the probability that the tail strike will occur based on a current descent trajectory of the aircraft and based on the one or more of the navigation data, the obstacle data, the engine data, or the terrain data, the control unit configured to direct the output device to present the alert to the pilot responsive to the probability that the tail strike will occur exceeding a threshold probability, and the control unit configured to instruct the pilot to follow one or more of a speed adjustment, provisional flight plan, a go-around procedure, and a missed approach procedure calculated responsive to the probability.
17 . The aircraft tail strike detection and prevention system of claim 16 , wherein the control unit is configured to calculate an alternate descent trajectory having one or more flare angles during descent that differ from the current descent trajectory and that reduces or eliminates the probability that the tail strike will occur upon touchdown during landing of the aircraft.
18 . The aircraft tail strike detection and prevention system of claim 17 , further comprising:
a flight control system configured to automatically control the aircraft to change the one or more flare angles according to the alternate descent trajectory during descent of the aircraft.
19 . The aircraft tail strike detection and prevention system of claim 16 , wherein the control unit is configured to calculate the go-around procedure for the aircraft to attempt another landing responsive to the probability that the tail strike will occur upon touchdown during landing of the aircraft using the alternate descent trajectory not decreasing below the threshold probability.
20 . The aircraft tail strike detection and prevention system of claim 16 , wherein the control unit is configured to calculate the probability based on one or more of aircraft gross weight, a landing weight, an amount or weight of fuel onboard the aircraft, a pitch angle or flare angle of the aircraft, positions of flaps of the aircraft, a windspeed and direction, or a runway condition.