Aircraft ground monitoring system

• US 4,122,522 A
• Filed: 06/02/1977
• Issued: 10/24/1978
• Est. Priority Date: 05/20/1974
• Status: Expired due to Term

• Current Assignee: Gerald R. Smith
• Original Assignee: Gerald R. Smith
• Inventors: Smith, Gerald R.
• Primary Examiner(s): Smith, Jerry
• Application Number:
  US05/802,662
• Time in Patent Office: 509 Days
• Field of Search: 235/150.2, 235/150.22, 340/26, 340/27 R, 73/178 T, 364/427, 364/428
• US Class Current: 701/15
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0026 located on the ground
• CPC Class Codes: G08G 5/0065 for taking-off
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

System for monitoring performance of an aircraft during ground-related operating condition, such as take-off and landing, to predict whether the aircraft can safely complete the operation. The performance of various known types of aircraft is predicted as a function of the distance which the aircraft has traveled along a runway. The actual progress of a known type of aircraft along a runway is then monitored to determine the actual velocity and position of the aircraft. Using the performance model for the known aircraft type, the remaining distance required for the aircraft to accomplish a particular operation, such as to reach take-off velocity or to decelerate to a stop, is predicted. The predicted distance is compared with the actual runway distance remaining for the aircraft to travel, and an alarm signal condition is generated if the actual remaining distance is less than the predicted required distance. The comparison is also made between the measured velocity of an aircraft moving along the runway and the predicted velocity which that type of aircraft should have attained, at various locations along the length of the runway. A warning signal is generated if the actual velocity is unacceptably different from predicted. The present system also predicts safe abort points conditions. Runway/taxiway intersection monitoring and control is also provided.

Claims

1. The method of predicting the performance of a specific aircraft of determinable certain type which is presently attempting to accomplish a particular flight operation along a runway, comprising the steps of:

prior to the present flight operation, measuring the actual velocities typically attained by aircraft of several types including said certain type, at particular distances while traveling along a runway in the successful accomplishment of a plurality of said particular flight operation, and then obtaining for each such type of aircraft an initial correlation signal between the distances which the aircraft have traveled with respect to a certain reference location of the runway and the typical velocities attained at such distances within a range of possible operating conditions during said plural flight operations, without regard to aircraft operating factors which may have affected the performance of said aircraft while traveling such distances to attain such velocities;

said initial correlation signals for each type of aircraft being represented by the equation;

space="preserve" listing-type="equation">V = B.sub.0 + B.sub.1 d + B.sub.2 d.sup.2 + B.sub.3 d.sup.3

where;

V is the average velocity at any distance d along the runway, and

B₀, B₁, B₂, and B₃ are constants determined from said typical velocity-distance information; and

then

at the time when said specific aircraft is attempting to accomplish said flight operation, identifying the aircraft type externally of said specific aircraft while said specific aircraft is traveling along the runway;

selecting said initial correlation signal which corresponds to said identified type of aircraft;

determining a signal which corresponds to the actual velocity of said specific aircraft at least at one known location of travel along the runway;

using said selected initial correlation signal to determine a signal corresponding to the anticipated velocity which an aircraft of said identified type should attain at said known location while attempting said flight operation;

comparing said anticipated velocity signal for said certain type of aircraft with said actual velocity signal of the specific aircraft to determine whether the normal velocity bears a predetermined relation to the actual velocity; and

providing a signal condition apparent to the operator of the specific aircraft if the anticipated velocity signal does not have said predetermined relationship with the known velocity signal.

2. The method as in claim 1, wherein said steps of determining the actual velocity signal for the specific aircraft, determining the anticipated velocity signal correlated with said known location of the specific aircraft, and comparing said anticipated velocity signal with said actual velocity signal take place externally of said specific aircraft.

3. The method as in claim 2, wherein:

said determination of an anticipated velocity signal for the specific aircraft is a first such determination made for a first known location of travel along said runway, and then

determining a signal which corresponds to the actual velocity as said specific aircraft travels to a second known location along said runway;

adjusting said selected initial correlation signal so that said initial correlation represented by said equation substantially coincides with said two actual distances of travel and the actual velocity signals, so that said adjusted correlation signal anticipates the velocity which said specific aircraft should have attained as a function of travel distance along the runway; and

then

using said adjusted correlation signal to determine the anticipated velocity of said specific aircraft for at least one additional runway location during said attempted flight operation.

4. The method as in claim 1, further comprising the steps of:

after said step of determining the actual velocity signal, then using said selected initial correlation signal to determine a distance signal correlated with said actual velocity signal to anticipate the distance which said identified type of aircraft should have traveled along the runway to attain said actual velocity;

comparing said anticipated distance for said identified type of aircraft with said reference location along the runway of the specific aircraft to determine whether the anticipated distance traveled bears a predetermined relation to the actual distance traveled; and

providing a signal condition apparent to the operator of the specific aircraft if the anticipated distance does not have said predetermined relationship with the actual distance.

5. The method as in claim 4, wherein:

said particular flight operation is a take-off;

said anticipated distance is a function of the the distance which said identified type of aircraft must travel from said known location to become airborne; and

said actual distance is a function of the length of the runway remaining from said known location.

6. The method as in claim 4, wherein:

said particular flight operation is a landing;

said anticipated distance is a function of the distance which said identified type of aircraft must travel from said known location to stop; and

said actual distance is a function of the length of runway remaining from said known location.

7. The method as in claim 1, wherein said constants B₀, B₁, B₂, and B₃ are determined from said typical information by least squares methodology.

8. The method of predicting the performance of a specific aircraft of determinable certain type which is presently attempting to accomplish a particular flight operation along a runway, comprising the steps of:

prior to the present flight operation, determining the velocities typically attained by aircraft of several types including said certain type at particular distances while traveling along a runway in the successful accomplishment of said particular flight operation, and then obtaining for each type of aircraft as initial correlation signal between the distances which the aircraft have traveled with respect to a certain reference location of the runway and the typical velocities attained at such distances within a range of possible operating conditions, without regard to aircraft operating factors which may have affected the performance of such aircraft while traveling such distances to attain such velocities;

said initial correlation signals for each type of aircraft being represented by the equation;

space="preserve" listing-type="equation">V = B.sub.0 + B.sub.1 d + B.sub.2 d.sup.2 + B.sub.3 d.sup.3

where;

V is the average velocity at any distance d along the runway, and

B₀, B₁, B₂, and B₃ are constants determined from said typical velocity-distance information; and

at the time when said specific aircraft is attempting to accomplish said flight operation,

identifying the aircraft type externally of said specific aircraft while said specific aircraft is traveling along the runway;

selecting said initial correlation signal which corresponds to said identified type of aircraft;

determining the actual velocity of said particular aircraft at least at one known location of travel along the runway;

using said selected initial correlation signal to determine the anticipated distance which an aircraft of said identified type should have traveled along the runway to attain said actual velocity;

comparing said anticipated distance for said certain type of aircraft with said actual location along the runway of the specific aircraft to determine whether the anticipated distance traveled bears a predetermined relation to the actual distance traveled; and

providing a signal condition apparent to the operator of the specific aircraft if the anticipated distance does not have said predetermined relationship with the actual distance.

9. The method as in claim 8, wherein said flight operation is an aircraft landing operation, said anticipated distance is the distance required to stop aircraft of the identified type, and said actual distance is the distance required to stop said specific aircraft.

10. The method as in claim 8, wherein said method steps take place externally of the aircraft.

11. The method of predicting the performance of a specific aircraft of determinable certain type which is presently attempting to accomplish a particular flight operation along a runway, comprising the steps of:

prior to the present flight operation, measuring the actual velocities typically attained by aircraft of several types, including said certain type, at particular distances while traveling along a runway in the successful accomplishment of a plurality of said particular flight operation, and then obtaining for separate each such type of aircraft an initial correlation signal between the distances which the aircraft have traveled with respect to a certain reference location of the runway and the velocities attained at such distances within a range of possible operating conditions during said plural flight operations, without regard to aircraft operating factors which may have affected the performance of said aircraft while traveling such distances to attain such velocities; and

then

at the time when said specific aircraft is attempting to accomplish said flight operation, identifying the aircraft type externally of said specific aircraft while said specific aircraft is traveling along the runway;

selecting said initial correlation signal which corresponds to said identified type of aircraft;

determining a signal which corresponds to the actual velocity of said specific aircraft at least at one known location of travel along the runway;

using said selected initial correlation signal to determine a signal corresponding to the anticipated velocity which an aircraft of said identified type should attain at said known location while attempting said flight operation;

comparing said anticipated velocity signal for said certain type of aircraft with said actual velocity signal of the specific aircraft to determine whether the normal velocity bears a predetermined relation to the actual velocity;

providing a signal condition apparent to the operator of the specific aircraft if the anticipated velocity signal does not have said predetermined relationship with the known velocity signal;

said determination of an anticipated velocity signal for the specific aircraft is a first such determination made for a first known location of travel along said runway, and then

determining a signal which corresponds to the actual velocity as said specific aircraft travels to a second known location along said runway;

adjusting said selected initial correlation signal to substantially coincide with said two actual distances of travel and the actual velocity signals, so that said adjusted correlation signal anticipates the velocity which said specific aircraft should have attained as a function of travel distance along the runway; and

then

using said adjusted correlation signal to determine the anticipated velocity of said specific aircraft for at least one additional runway location during said attempted flight operation.