Airplane take-off monitor with learning feature

• US 4,980,833 A
• Filed: 07/26/1988
• Issued: 12/25/1990
• Est. Priority Date: 07/26/1988
• Status: Expired due to Term

• Current Assignee: Mancil W. Milligan, Wilkerson H. Joe
• Original Assignee: The University Of Tennessee Research Corporation (University of Tennessee)
• Inventors: Wilkerson, H. Joe, Milligan, Mancil W.
• Primary Examiner(s): Black, Thomas G.
• Application Number:
  US07/224,492
• Time in Patent Office: 882 Days
• Field of Search: 364/427, 364/428, 364/424.06, 364/433, 73/178 T, 340/972, 244/183
• US Class Current: 701/15
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase

Abstract

A take-off performance monitor uses a sensor to produce a movement signal proportional to the movement of an aircraft during a take-off roll and, for each take-off, historical data is generated and stored based on the movement signal. An analyzing unit of the monitor uses the historical data and current conditions to calculate a reference take-off distance, reference acceleration data and reference velocity data. This information is output to the pilor to facilitate his judgment as to the adequacy to take-off performance. In the preferred embodiment, the analyzing unit utilizes five samples of acceleration and velocity during a take-off roll to solve an equation for five constants that are indicative of take-off performance. The five constants relate to static thrust, a linear relationship between thrust and velocity, a non-linear relationship between thrust and velocity, air drag and rolling drag, and these five constants constitute at least part of the historical data. During an actual take-off the actual acceleration of the aircraft and the reference acceleration are displayed to allow the pilot to make a quantitative evaluation of the takeoff performance. This comparison can be made at velocities much below take-off velocity and thus will allow a safe abortion of abnormal take-offs. In addition to an acceleration comparison a live take-off distance, based on actual take-off acceleration, is displayed and compared to the reference take-off distance as predicted in part from historical data.

Claims

1. A take-off performance monitor for an aircraft comprising:

means for inputting parameters affecting the take-off performance of the aircraft including at least environmental factors and engine power settings;

storage means for storing said parameters;

means for measuring the movement of the aircraft during a take-off roll to produce a movement signal;

means responsive at least to said movement signal for determining at least the aircraft acceleration and a corresponding aircraft velocity and for producing aircraft acceleration and velocity data;

said storage means being operable to store said aircraft acceleration and velocity data;

calculating means responsive to the input parameters and the aircraft acceleration and velocity data for calculating at least one take-off constant based upon both the input parameters and the acceleration and velocity data, said take-off constant being indicative of aircraft take-off performance;

said storage means including stored historical data corresponding to said at least one take-off constant for at least selected take-offs of the aircraft;

analyzing means for analyzing take-off performance substantially in real-time during a take-off roll by using the historical data collected from previous take-offs and the current take-off performance to produce analyzed data; and

output means for outputting the analyzed data to the pilot.

2. The monitor of claim 1 wherein said analyzing means further comprises:

predicting means for producing a reference take-off performance based on the input parameters and the historical data in said storage means;

means for monitoring the acceleration and velocity and determining actual take-off performance; and

means for outputting data corresponding to the reference take-off performance and the actual take-off performance.

3. The monitor of claim 1 wherein said storage means further comprises means for calculating at least one average take-off constant based on at least one take-off constant determined for each of plurality of take-offs.

4. The monitor of claim 1 wherein said calculating means further comprises means for calculating a plurality of take-off constants for each take-off.

5. The monitor of claim 1 wherein said analyzing means further comprises predicting means for predicting a reference take-off distance based on the input parameters and the historical data and for predicting a live take-off distance during a take-off roll based on the input parameters and the movement signal;

and

means for outputting data corresponding to the reference take-off distance and the live take-off distance during the take-off roll.

6. The monitor of claim 1 wherein said analyzing means further comprises:

predicting means for calculating a reference acceleration of the aircraft at each of a plurality of velocities based upon the historical data and the input parameters;

means for determining actual acceleration and velocity of the aircraft during the take-off roll from the movement signal; and

means for outputting data corresponding to the reference acceleration and the actual acceleration for the actual velocity during the take-off roll.

7. The monitor of claim 1 wherein said analyzing means comprises:

predicting means for calculating a reference velocity of the aircraft for a plurality of distances in a take-off roll based upon the historical data and the input parameters;

means for determining the actual velocity and actual roll distance of the aircraft during the take-off roll from the movement signal; and

means for outputting the data corresponding to the reference velocity and the actual velocity during the take-off roll at the actual roll distance.

8. The apparatus of claim 1 wherein said storage means stores data corresponding to a plurality of take-off constants calculated from a plurality of take-offs whereby changes in the aircraft take-off performance over time can be detected by comparing changes over a period of time in the data corresponding to the take-off constants.

9. A take-off performance monitor for an aircraft in which the aircraft has air drag, rolling drag and a thrust setting apparatus for setting static and dynamic thrust of the aircraft, said monitor comprising:

means for inputting parameters affecting take-off performance of the aircraft including parameters indicative of percentage of rated thrust for a particular take-off, aircraft weight, headwind velocity, air temperature, runway slope and atmospheric pressure;

storage means for storing said parameters;

means for measuring the movement of the aircraft during a take-off roll to produce a movement signal;

means responsive at least to said movement signal for determining at least the actual acceleration and velocity of the aircraft during the take-off roll and for producing at least aircraft actual acceleration and velocity data;

said storage means being operable to store said aircraft actual acceleration and velocity data;

calculating means responsive to the input parameters and the aircraft actual acceleration and velocity data to solve an aircraft performance equation to determine X number of equation constants, said calculating means being operable to solve said equation based on X number of actual acceleration values and X number of corresponding actual velocity values;

said storage means including stored historical data corresponding the X number of equation constants for a plurality of previous take-offs;

means for predicting a reference take-off performance for a particular take-off based at least upon the input parameters and the historical data to produce reference data; and

means for outputting the reference data to the pilot.

10. The apparatus of claim 9 wherein said calculating means further comprises means for solving the equation to determine at least one constant relating to static thrust of the aircraft.

11. The monitor of claim 9 wherein said calculating means further comprises means for solving the equation to determine at least one constant relating to dynamic thrust of the aircraft.

12. The monitor of claim 9 wherein said calculating means further comprises means for solving the equation to determine at least one constant relating to air drag of the aircraft.

13. The monitor of claim 9 wherein said calculating means further comprises means for solving the equation to determine at least one constant relating to rolling drag of the aircraft.

14. The monitor of claim 9 wherein said calculating means further comprises means for solving the equation to determine at least three constants relating to thrust, the first such constant relating to the static thrust of the aircraft, the second such constant relating to a linear relationship between thrust and velocity, and the third constant relating to a non-linear relationship between thrust and velocity.

15. The monitor of claim 9 wherein said calculating means further comprises means for solving the following equation:

space="preserve" listing-type="equation">a=1/W{A(C1)(V.sub.G +V.sub.W)+[A(C3)-(C4)P/T +(C5)μ

P/T][V.sub.G +V.sub.2 ].sup.2 -μ

g W cos θ

-g W sin θ

} (Equation

     1)

Inputs which the pilot would have to make include;

A--percent of rated thrust or power

W--aircraft gross weight at take-off

V_W --headwind component (maybe generated from runway heading and wind direction and velocity)

T--outside air temperature (OAT)

P--atmospheric pressure

μ

--coefficient of rolling resistance

θ

--runway slope

and where;

g=acceleration due to gravity

a=aircraft acceleration

V_G =aircraft ground velocity

to determine five constants, C1, C2, C3, C4, and C5 wherein C1 relates to static thrust;

C2 relates to linearly changing thrust with velocity, C3 relates to non-linearly changing thrust with velocity, C4 relates to air drag and C5 relates to rolling drag.