Flight management system providing minimum total cost

• US 4,760,530 A
• Filed: 06/17/1986
• Issued: 07/26/1988
• Est. Priority Date: 06/17/1986
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Liden, Sam P.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black, Thomas G.
• Application Number:
  US06/875,115
• Time in Patent Office: 770 Days
• Field of Search: 364/442, 364/433, 364/434, 364/440, 364/439, 364/427, 364/428, 364/430, 364/148, 364/431.07, 364/431.01, 244/178, 244/180, 73/178 T
• US Class Current: 701/123
• CPC Class Codes: G05D 1/0005 with arrangements to save energy

Abstract

A flight management system that provides an airspeed command to control a flight profile pursuant to minimum total cost. Total cost is the sum of direct operating cost and arrival time error cost and direct operating cost is the sum of fuel cost plus flight-time cost. A predictor, in response to trial cost index values, generates direct operating cost and arrival time values corresponding to the trial cost index values. A parabolic function approximator generates a parabolic approximation to the direct operating cost vs. arrival time function corresponding to the trial cost index values. An arrival error cost function is added to the direct operating cost function and the minimum of the combined function is obtained to provide an optimum arrival time signal. The trial cost index values and the corresponding arrival time values are applied to a parabolic approximator to obtain a cost index vs. arrival time function. The optimum arrival time signal is applied to this function to provide the optimum cost index signal corresponding thereto. A speed generator is included for generating an airspeed signal corresponding to the optimum cost index signal in accordance with minimum direct operating cost. A predictor generates a predicted arrival time signal in accordance with the optimum cost index signal. A speed adjuster adjusts the airspeed signal to provide the airspeed command signal in accordance with the difference between the optimum arrival time signal and the predicted arrival time signal.

Claims

1. Flight Management System apparatus for aircraft comprising

means for generating a DOC signal which is a function of direct operating cost (DOC) versus arrival time in accordance with a range of cost index values,

means for storing values of arrival time error cost (AEC) versus arrival time error and providing an AEC signal which is function of said values,

means for combining said DOC signal with said AEC signal to provide a total flight cost signal which is a function of total flight cost, thereby establishing a signal representative of total flight cost versus arrival time,

minimizing means responsive to said total flight cost signal for determining a minimum thereof to provide an optimum arrival time signal,

means responsive to said optimum arrival time signal for providing an optimum cost index signal corresponding thereto,

speed generator means responsive to said optimum cost index signal for generating an airspeed signal corresponding thereto in accordance with minimum direct operating cost,

predictor means responsive to said optimum cost index signal for generating a predicted arrival time signal in accordance therewith, and

speed adjuster means responsive to said optimum arrival time signal, said predicted arrival time signal and said airspeed signal for adjusting said airspeed signal in accordance with the difference between said optimum arrival time signal and said predicated arrival time signal to provide an airspeed command signal for controlling the airspeed of said aircraft.

2. The apparatus of claim 1 wherein said DOC signal generating means comprises

means for providing a plurality of trial cost index value signals,

further predictor means responsive to each of said trial cost index value signals for generating a further predicted arrival time signal and a further DOC signal in accordance with said further predicted arrival time, and

means responsive to said further predicted arrival time signal and said further DOC signal corresponding to each of said trial cost index value signals for generating said DOC signal in accordance with said further predicted arrival time signals and said further DOC signals.

3. The apparatus of claim 2 in which said means responsive to said further predicted arrival time signal and said further DOC signal comprises polynomial estimating means responsive to said further predicted arrival time signal and said further DOC signal corresponding to each of said trial cost index value signals for generating a polynomial estimate curve in accordance with said further predicted arrival time signals and said further DOC signals.

4. The apparatus of claim 3 in which said polynomial estimating means comprises a estimator for generating a parabolic estimate of said DOC signal.

5. The apparatus of claim 3 in which said DOC signal generating means, said storing means and said combining means comprise means for generating said signal representative of total flight cost versus arrival time.

6. The apparatus of claim 5 in which said minimizing means comprises search means for providing trial arrival time signals to said total flight cost versus arrival time signal generating means so as to activate said total flight cost versus arrival time signal generating means to provide to said search means values of total flight cost corresponding to said trial arrival time signals.

7. The apparatus of claim 6 in which said search means comprises means for comparing successive values of said total flight time costs corresponding to successive values of said trial arrival time signals for determining the trial arrival time signal corresponding to the minimum value of said total flight time costs.

8. The apparatus of claim 7 in which said search means further includes

means for providing a minimum-not signal representative of a minimum total flight cost value not being detected, and

means for providing a direction signal representative of whether said trial arrival time signals are increasing or decreasing when said minimum-not signal is generated.

9. The apparatus of claim 8 in which said trial cost index value signal providing means is responsive to said minimum-not signal and said direction signal for providing an additional trial cost index value signal to extend said polynomial estimate curve in the direction of the minimum thereof.

10. The apparatus of claim 8 in which said storing means comprises means for storing said AEC values with critical time points in accordance with connecting flight times.

11. The apparatus of claim 10 in which said trial arrival time signals include said critical time points.

12. The apparatus of claim 3 in which said means responsive to said optimum arrival time signal comprises means further responsive to said trial cost index value signals and said further predicted arrival time signals for generating a polynomial estimate curve in accordance therewith.

13. The apparatus of claim 2 in which said further predictor means comprises

further speed generator means responsive to each of said trial cost index value signals for generating an airspeed signal corresponding thereto in accordance with minimum direct operating cost,

a predictor responsive to said airspeed signal from said further speed generator means for providing a predicted arrival time signal and a predicted fuel burn signal in accordance therewith, and

a DOC generator responsive to said predicted arrival time signal and said predicted fuel burn signal from said predictor and further responsive to said input cost index value signal representative of unit cost of fuel for generating said further DOC signal in accordance therewith.

14. The apparatus of claim 13 in which said DOC generator comprises means for generating said further DOC signal in accordance with

15. The apparatus of claim 1 in which said means for storing comprises means for storing said AEC values with critical time points in accordance with connecting flight times.

16. The apparatus of claim 1 in which said means for combining comprises means for adding said AEC signal to said DOC signal to provide said total flight cost signal.

17. The apparatus of claim 1 in which said DOC signal generating means, said storing means and said combining means comprise means for generating said signal representative of total flight cost versus arrival time.

18. The apparatus of claim 17 in which said minimizing means comprises search means for providing trial arrival time signals to said total flight cost versus arrival time signal generating means so as to activate said total flight cost versus arrival time signal generating means to provide signals to said search means representative of values of total flight cost corresponding to said trial arrival time signals.

19. The apparatus of claim 18 in which said search means comprises means for comparing successive values of said total flight time costs corresponding to successive values of said trial arrival time signals for determining the trial arrival time signal corresponding to the minimum value of said total flight time costs.

20. The apparatus of claim 19 in which said search means further includes

means for providing a minimum-not signal representative of a minimum total flight cost value not being detected, and

means for providing a direction signal representative of whether said trial arrival time signals are increasing or decreasing when said minimum-not signal is generated.

21. The apparatus of claim 1 in which said speed generator means includes means for providing measured aircraft and atmosphere parameter signals to said speed generator means for generating said airspeed signal in accordance with minimum direct operating cost.

22. The apparatus of claim 21 in which said predictor means includes means for providing simulated aircraft and atmosphere parameter signals, corresponding to said measured aircraft and atmosphere parameter signals to said predictor means for generating said predicted arrival time signal in accordance with said optimum cost index signal.

23. The apparatus of claim 22 in which said predictor means comprises means for generating said predicted arrival time signal, a T_UP signal and a T_DN signal, where said T_UP and T_DN signals represent predicted flight time adjusted for time segments having speed or acceleration limits associated therewith.

24. The apparatus of claim 23 in which said speed adjuster means comprises

a speed adjustment factor generator responsive to said optimum arrival time signal and said predicted arrival time signal for generating a speed adjustment factor signal in accordance with the difference therebetween, and

a speed adjuster responsive to said airspeed signal and said speed adjustment factor signal for providing said airspeed command signal in accordance therewith.

25. The apparatus of claim 24 in which said speed adjustment factor generator comprises means responsive to said T_UP and T_DN signals for generating said speed adjustment factor further in accordance with a selected one of said T_UP and T_DN signals.

26. The apparatus of claim 25 in which said speed adjustment factor generator comprises means for generating said speed adjustment factor signal in accordance with

27. The apparatus of claim 26 in which said speed adjuster comprises means responsive to a measured wind signal for further adjusting said airspeed signal in accordance therewith.

28. The apparatus of claim 27 further including means for generating an activation signal for activating said DOC signal generating means, said speed adjustment factor generator being responsive to said activation signal for setting K_SA to zero when said DOC signal generating means is activated.

29. The apparatus of claim 26 in which said speed adjuster comprises means for providing said airspeed command signal in accordance with

30. A flight management system method for aircraft comprising the steps of

generating a function of direct operating cost (DOC) vs. arrival time in accordance with a range of cost index values,

storing a function of arrival time error cost, (AEC) vs. arrival time error,

combining said DOC function with said AEC function to provide a function of total flight cost vs. arrival time,

determining the minimum of said total flight cost vs. arrival time function to provide an optimum arrival time signal,

providing an optimum cost index signal corresponding to said optimum arrival time signal,

generating an airspeed signal corresponding to said optimum cost index signal in accordance with minimum direct operating cost,

generating a predicted arrival time signal in accordance with said optimum cost index signal, and

adjusting said airspeed signal in accordance with the difference between said optimum arrival time signal and said predicted arrival time signal to provide an airspeed command signal for controlling the airspeed of said aircraft.