Hierarchical target intercept fuzzy controller with forbidden zone

• US 5,944,762 A
• Filed: 04/01/1996
• Issued: 08/31/1999
• Est. Priority Date: 04/01/1996
• Status: Expired due to Fees

• Current Assignee: Navy Department United States of America The As Represented By The Secretary of The Navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Bessacini, Anthony F., Pinkos, Robert F.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US08/627,764
• Time in Patent Office: 1,247 Days
• Field of Search: 701/1, 701/23, 701/27, 701/302, 395/3, 395/900, 395/905, 318/589, 244/3.1, 244/3.11, 244/3.13, 244/3.14, 244/3.15, 244/3.19
• US Class Current: 701/27
• CPC Class Codes: F41G 7/306 for transmitting guidance signals; F41G7/308 takes precedence
• CPC Class Codes: F42B 19/01 Steering control

Abstract

A target intercept guidance system for directing a steerable object, such a torpedo with a guidance point. The guidance system is located at a launching vehicle and senses the bearings from the launching vehicle to a target and to the steerable object as it moves toward the target. Various error signals are then generated and classified into sensed linguistic variables using membership functions of corresponding sensed variable membership function sets based upon primary and secondary goals to become fuzzy inputs that produce fuzzy control output membership functions from a control output membership function set based upon logical manipulation of the fuzzy inputs. The control system performs this classification and selection according to sometimes competing goals of excluding the torpedo from a particular operating zone while guiding the torpedo in response to variations in a target bearing relative to the guidance point. The selected fuzzy control output membership functions are converted into an output having an appropriate form for control, subject to optional conditioning to prevent unwanted effects and assure good behavior for different tactical parameters.

Claims

1. In a hierarchial control system for guiding a steerable object from a launching vehicle toward a target in response to multiple goal control rules based upon signals from sensing means corresponding to bearings from the launching vehicle to the steerable object and to the target and from the steerable object to the target wherein said steerable object is characterized by a center point and by a guidance point externally of the steerable object and leading the steerable object as it moves toward the target, said hierarchial control system comprising:

first error means for generating first sensed variable signals in response to the signals from said sensing means indicating the location of the steerable object with respect to a zone about a line between the launching vehicle and the target;

second error means for generating second sensed variable signals in response to the signals from said sensing means indicating whether the bearing from the guidance point to the target is varying with time;

sensed variable means for converting the first and second sensed variable signals into corresponding first and second sensed linguistic variables using corresponding first and second sensed variable membership functions;

control output means for producing a command signal for guiding the steerable object from the launching vehicle toward the target in response to the selection of a control output membership function; and

multi-goal rule based means interposed between said sensed variable means and said control output means for selecting said control output membership function in accordance with one of the competing multiple output control rules selected by said multi-goal rule based means in response to the first sensed variable membership functions.

2. A hierarchial control system as recited in claim 1 wherein said first error means includes:

means for determining an angular difference between the bearings from the launching vehicle to the target and to the steerable object and an angular separation about the sensed bearing from the launching vehicle to the target; and

means for determining the rate of change of the angular difference and wherein said first sensed linguistic variables and said first membership function sets correspond to the angular difference and the rate of change of the angular difference.

3. A hierarchial control system as recited in claim 2 wherein said sensing means produces a bearing from the guidance point of the steerable object to the target and a course of the steerable object, said second error means selecting said second sensed linguistic variables using corresponding membership functions based upon the difference between the bearing from the guidance point to the target and the course of the steerable object and based upon the rate of change of the difference between the bearing from the guidance point to the target and the course.

4. A hierarchial control system as recited in claim 3 wherein said angular difference determining means generates an angular error signal corresponding to the difference between the bearings from the launching vehicle to the steerable object and from the launching vehicle to the target and an angular separation about the bearing from the launching vehicle to the target to determine whether the steerable object is located within the zone and a rate of change error signal corresponding to the rate of change of bearing signal differences.

5. A hierarchial control system as recited in claim 4 wherein a zone defining means defines the zone as a function of range from the launching vehicle along the bearing to the target object.

6. A hierarchial control system as recited in claim 5 additionally comprising command signal conditioning means for modifying the command signal from said control output means.

7. A hierarchial control system as recited in claim 6 wherein said command conditioning means includes gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target.

8. A hierarchial control system as recited in claim 6 wherein said command conditioning means includes constraint means for limiting the magnitude of the command signal.

9. A hierarchial control system as recited in claim 6 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting one of said gain adjustment means and said constraint means for conditioning the command signal.

10. A hierarchial control system as recited in claim 6 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting said constraint means when the range between said guidance point and the target exceeds a predetermined multiple of the distance between the center and the guidance point of the steerable object and selects said gain adjustment means when the range is less than the predetermined multiple.

11. A hierarchial control system as recited in claim 6 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting said constraint means when the range between said guidance point and the target exceeds a predetermined value of about 1.5 times the distance between the center and the guidance point of the steerable object and selects said gain adjustment means when the range is less than a predetermined multiple.

12. A hierarchial control system as recited in claim 1 additionally comprising command signal conditioning means for modifying the command signal from said control output means.

13. A hierarchial control system as recited in claim 12 wherein said command conditioning means includes gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target.

14. A hierarchial control system as recited in claim 12 wherein said command conditioning means includes constraint means for limiting the magnitude of the command signal.

15. A hierarchial control system as recited in claim 12 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude range of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting one of said gain adjustment means and said constraint means for conditioning the command signal.

16. A hierarchial control system as recited in claim 12 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting said constraint means when the range between said guidance point and the target exceeds a predetermined multiple of the distance between the center and the guidance point of the steerable object and selects said gain adjustment means when the range is less than the predetermined multiple.

17. A hierarchial control system as recited in claim 12 wherein said command conditioning means includes:

gain adjustment means for adjusting the gain of the command signal in response to the range between the guidance point and the target;

constraint means for limiting the magnitude of the command signal; and

selection means responsive to signals indicating the range between the guidance point and the target for selecting said constraint means when the range between said guidance point and the target exceeds a predetermined value of about 1.5 times the distance between the center and the guidance point of the steerable object and selects said gain adjustment means when the range is less than a predetermined multiple.

18. An iterative method for guiding a steerable object from a launching vehicle to a target in response to any of competing sets of multiple goal control rules based upon signals from sensing means corresponding to bearings from the launching vehicle to the steerable object and to the target and from the steerable object to the target wherein the steerable object is characterized by a center point and by a guidance point externally of the steerable object and leading the steerable object as it travels toward the target wherein each said iteration comprises the steps of:

generating first sensed variable signals in response to the signals from the sensing means indicating the location of the steerable object with respect to a zone about a line between the launching vehicle and the target;

generating second sensed variable signals in response to the signals from the sensing means indicating whether the bearing from the guidance point of the steerable object to the target is varying with time;

retrieving first and second sensed linguistic variables in response to the first and second sensed variable signals, respectively;

selecting at least one control output linguistic variable from a predetermined set of control output linguistic variables in response to the selected first or second sensed linguistic variables from the first set when the first sensed variable signals indicate that the steerable object is proximate or inside the predetermined zone and in response to the second set when the sensed variable signals indicate that the steerable object is outside the predetermined zone;

generating a command signal for controlling the steerable object in response to a control output linguistic variables selection; and

transferring the command signal to the steerable object.

19. A method as recited in claim 18 wherein the step of generating the first sensed variable signals includes the steps of:

determining an angular difference between the bearings from the launching vehicle to the target and to the steerable object and an angular separation about the sensed bearing from the launching vehicle to the target; and

determining the rate of change of the angular difference and wherein the first sensed linguistic variables and said first membership function sets correspond to the angular difference and the rate of change of the angular difference.

20. A method as recited in claim 19 wherein the step of generating the second sensed variable signals includes determining a bearing from the guidance point to the target and selecting corresponding second sensed linguistic variables based upon the difference between the bearing from the guidance point to the target and the course of the steerable object and based upon the rate of change of the difference between the bearing from the guidance point to the target and the course.

21. A method as recited in claim 20 wherein said step of determining angular difference includes generating a angular error signal corresponding to the difference between the bearings from the launching vehicle to the steerable object and to the target and an angular separation about the bearing from the launching vehicle to the target thereby to indicate whether the steerable object is located within a zone about the bearing from the launching vehicle to the target and a rate of change error signal corresponding to the rate of change of the bearing signal differences.

22. A method as recited in claim 21 further comprising a step of defining the zone includes defining the zone as a function of range from the launching vehicle along the bearing to the target object.

23. A method as recited in claim 22 wherein the step of generating the command signal includes the step of modifying the command signal from the control output linguistic variable selection.

24. A method as recited in claim 23 wherein said step of modifying the command signal includes the step of adjusting the gain of the command signal in response to the range between the guidance point and the target.

25. A method as recited in claim 23 wherein said step of modifying the command signal includes the step of constraining the magnitude of the command signal.

26. A method as recited in claim 23 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.

27. A method as recited in claim 23 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions when the sensed variable signals indicate that the range between the guidance point and the target is less than a predetermined multiple of the distance between the center and the guidance point of the steerable object, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.

28. A method as recited in claim 23 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions when the sensed variable signals indicate that the range between the guidance point and the target is less than 1.5 times the distance between the center and the guidance point of the steerable object, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.

29. A method as recited in claim 18 wherein the step of generating the command signal includes the step of modifying the command signal from the control output linguistic variable selection.

30. A method as recited in claim 18 wherein said step of modifying the command signal includes the step of adjusting the gain of the command signal in response to the range between the guidance point and the target.

31. A method as recited in claim 29 wherein said step of modifying the command signal includes the step of constraining the magnitude of the command signal.

32. A method as recited in claim 29 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.

33. A method as recited in claim 29 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions when the sensed variable signals indicate that the range between the guidance point and the target is less than a predetermined multiple of the distance between the center and the guidance point of the steerable object, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.

34. A method as recited in claim 29 wherein said step of modifying the command signal includes the step of modifying the command signal by:

selecting, under first conditions when the sensed variable signals indicate that the range between the guidance point and the target is less than 1.5 times the distance between the center and guidance points of the steerable object, a step of adjusting the gain of the command signal in response to the range between the guidance point and the target; and

selecting, under other conditions, a step of constraining the magnitude of the command signal.