Feature navigation system and method

• US 4,700,307 A
• Filed: 07/11/1983
• Issued: 10/13/1987
• Est. Priority Date: 07/11/1983
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: General Dynamics Corporation
• Inventors: Mons, Barend, Henderson, Robert L., Flowers, Donald H.
• Primary Examiner(s): CANGIALOSI, SALVATORE A
• Application Number:
  US06/514,210
• Time in Patent Office: 1,555 Days
• Field of Search: 364/453, 364/456, 364/457, 358/103, 343/5 MM, 342/64, 342/54, 342/55
• US Class Current: 701/220
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft

Abstract

A method of navigating an airborne vehicle using observation of linear features such as roads, railroads, rivers or the like. Maps of linear features in several discrete areas along an intended flight path are prepared and entered into an on-board computer memory. The vehicle typically uses an inertial navigation system during flight from the origin to the first mapped area. Imaging sensors and on-board processing detect linear features as the vehicle approaches or passes over them. The sensed feature pattern network is compared to the reference mapped feature network to update the inertial navigation system to generate guidance commands. Frequent updates at other mapped areas keep the vehicle on course. This system is also capable of navigation updates from single linear features when the flight path is fairly well known, and of tracking a linear feature for terminal guidance. In these cases, only a small number of feature parameters need to be stored, rather than an area map. Linear feature navigation can be used by any manned or unmanned airborne vehicle which has the on-board capability to detect the required features.

Claims

1. A method of airborne vehicle navigation using linear feature orientation which consists of the steps of:

preparing a map of extended, substantially one-dimensional linear features along a path to be flown;

flying the airborne vehicle along the initial portion of said path;

detecting the location and direction of said linear features as said vehicle flys over them;

comparing the locations and directions of the detected features relative to the corresponding features on the map;

determining the actual location of the vehicle relative to the center of the intended flight path; and

correcting the actual vehicle flight path to return to the intended path.

2. The method according to claim 1 wherein said detection is accomplished by an active sensor looking ahead of the vehicle flight path.

3. The method according to claim 1 wherein said detection is accomplished by laser radar ranging ahead of said vehicle.

4. The method according to claim 1 wherever said detection is accomplished by a passive sensing means sensing the area immediately below the vehicle.

5. The method according to claim 1 wherein said detection is accomplished by a television imaging system directed below the vehicle.

6. The method according to claim 1 wherein said vehicle is navigated from launch to the first linear feature navigation correction and between and subsequent corrections by inertial navigation methods.

7. The method according to claim 1 wherein said corrections are made from about 1 to 120 times per hour of flight.

8. A method of airborne vehicle navigation using linear feature sequence matching which consists of:

preparing a map of extended, substantially one-dimensional linear features along a selected path to be flown;

flying an airborne vehicle along the initial portion of said path;

detecting linear ground features as the vehicle crosses them;

recording the current position as each feature is crossed, the distances between each pair of crossings and the vehicle movement direction between each pair of crossings to produce an X, Y vector distance between each pair of crossings;

shifting the map network between each pair of crossings through the vector distance;

recording all intersection positions between the shifted and unshifted maps;

accumulating votes at each position through a plurality of successive crossings;

projecting forward the votes from earlier crossings to the N^th crossing;

whereby the position having the most votes at the N^th crossing is the actual location;

correcting the actual vehicle flight path to return the vehicle to the desired flight path.

9. The method according to claim 8 wherein said detection is accomplished by an active sensor looking ahead of the vehicle flight path.

10. The method according to claim 8 wherein said detection is accomplished by laser radar ranging ahead of said vehicle.

11. The method according to claim 8 wherever said detection is accomplished by a passive sensing means sensing the area immediately below the vehicle.

12. The method according to claim 8 wherein said detection is accomplished by a television imaging system directed below the vehicle.

13. The method according to claim 8 wherein said vehicle is navigated from launch to the first linear feature navigation correction and between and subsequent corrections by inertial navigation methods.

14. A method of airborne vehicle navigation using linear feature tracking which consists of:

preparing a map of extended, substantially one-dimensional linear features along a selected path to be flown;

flying an airborne vehicle along at least the initial portion of said path until a selected linear feature is approached which extends to the vehicle destination;

sensing said selected linear feature when reached by said vehicle;

guiding said vehicle along said selected linear feature; and

continuing flight until said destination is reached.

15. The method according to claim 14 wherein:

said selected linear feature passes near, but not directly to, the vehicle destination;

as said vehicle is guided toward the destination vicinity along said selected feature, detecting an anomaly in said selected feature near said destination;

at a selected distance from said anomaly, turning the flight path of said vehicle through a selected angle to cause said vehicle to fly directly to said destination.

16. The method according to claim 15 wherein said sensing is accomplished by a television imaging system directed forward of vehicle.

17. The method according to claim 15 wherein said vehicle is navigated from launch to the first linear feature navigation correction and between and subsequent corrections by inertial navigation methods.

18. A system for airborne vehicle navigation using linear feature orientation which comprises:

sensor means for detecting the presence and orientation of extended, substantially one-dimensional linear feature on the surface of the earth as the sensor-bearing airborne vehicle encounters them;

a reference map of linear features along a corridor which includes the intended flight path;

means for comparing the sensed linear feature locations and orientations to features on said map;

means for correlating the sensed features and mapped features to determine the actual location and flight path of the vehicle; and

means for correcting the vehicle flight path to return to the intended flight path.

19. The system according to claim 18 wherein said sensor means comprises a laser radar ranging ahead of said vehicle.

20. The system according to claim 18 wherein said sensor means comprises a television imaging system sensing the area immediately forward of the vehicle.

21. The system according to claim 18 features including inertial navigation means for navigating the vehicle between linear feature navigation updates.

22. In a navigation system for an unmanned airborne vehicle which comprises vehicle propulsion and steering means for flying said vehicle along a selected path, an inertial navigation system for guiding said vehicle approximately along said path, the improvement comprising linear feature orientation means for updating and correcting said inertial navigation system, said orientation means comprising:

sensor means for detecting the presence and orientation of linear feature on the surface of the earth as the sensor-bearing airborne vehicle encounters them;

a reference map of linear features along a corridor which includes the intended flight path;

means for comparing the sensed linear feature locations and orientations to features on said map;

means for correlating the sensed features and mapped features to determine the actual location and flight path of the vehicle; and

means for correcting the vehicle flight path to return to the intended flight path.

23. The system according to claim 22 wherein said sensor means comprises a laser radar ranging ahead of said vehicle.

24. The system according to claim 22 wherein said sensor means comprises a television imaging system sensing the area immediately forward of the vehicle.

25. The system according to claim 22 wherein said comparison means comprises:

means for recording the current position as each sensed linear feature is crossed by said vehicle, the distance between each pair of crossings and the vehicle movement direction between each pair of crossings to produce an X, Y, vector distance between each pair of crossings;

means for shifting the map network between each pair of crossings through the vector distance and recording all intersection positions between the shifted and unshifted maps;

means for accumulating votes at each position through a plurality of successive crossings and projecting forward the votes from the earlier crossings to the N^th crossing to determine that the position with the most votes is the actual position; and

means for directing the actual position information to void inertial navigation undating and connecting means.