Computerized flight inspection system

• US 4,792,904 A
• Filed: 01/06/1988
• Issued: 12/20/1988
• Est. Priority Date: 06/17/1987
• Status: Expired due to Fees

• Current Assignee: Sienna Technologies, Inc.
• Original Assignee: LTV Aerospace and Defense Company
• Inventors: Johnson, Allen B., Reinagel, Frederick G.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US07/140,875
• Time in Patent Office: 349 Days
• Field of Search: 364/428-430, 364/439, 364/443, 364/456, 364/571, 358/103, 340/947, 340/948, 340/951, 340/953, 340/954, 340/955, 340/956, 73/178 T
• US Class Current: 701/17
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01S 17/88 Lidar systems specially adapted for specific applications
• CPC Class Codes: G05D 1/0676 specially adapted for landing

Abstract

A computerized flight inspection system is disclosed. The system of the present invention may be utilized to generate an accurate reference location with respect to an airport runway for an aircraft having an inertial navigation system. A selected geometric pattern having a highly unambiguous autocorrelation function is placed on at least one end of the runway. A video line scanning camera mounted to the aircraft is then utilized to scan the geometric pattern in a line generally perpendicular to the line of flight. The output of the video line scanning camera is then correlated with a stored reference pattern to generate a signal indicative of the detection of the geometric pattern on the runway. A laser altimeter is mounted to the aircraft and utilized to generate an accurate signal indicative of the aircraft altitude with respect to the runway pattern. The outputs of the correlation circuit and the laser altimeter are then utilized to correct data from the inertial navigation system.

Claims

1. A computerized flight inspection system for providing an accurate reference location with respect to a runway for an aircraft having an inertial navigation system, said flight inspection system comprising:

selected indicia disposed on at least one end of an airport runway;

video scanning means disposed within said aircraft for scanning said selected indicia in a line generally perpendicular to said aircraft'"'"'s line of flight and for generating an output indicative of the scanned video pattern;

memory means for storing a reference video pattern;

correlator means coupled to said video scanning means and said memory means for correlating said scanned video pattern and said reference video pattern;

altimeter means for measuring the altitude of said aircraft and for generating a signal indicative thereof; and

processor means coupled to said correlator means and said altimeter means for generating correction data for said inertial navigation system in response to said correlation and said altitude measurement.

2. The computerized flight inspection system according to claim 1 wherein said selected indicia comprises a selected geometric pattern.

3. The computerized flight inspection system according to claim 1 wherein said video scanning means comprises a solid state line scan camera.

4. The computerized flight inspection system according to claim 3 wherein said solid state line scan camera includes a charge couple device line scan image sensor.

5. The computerized flight inspection system according to claim 4 wherein said charge couple device line scan image sensor includes a single row of 1,024 image sensing elements.

6. The computerized flight inspection system according to claim 1 wherein said correlator means comprises a sixty-four bit monolithic digital correlator.

7. The computerized flight inspection system according to claim 1 wherein said altimeter means comprises a laser altimeter.

8. The computerized flight inspection system according to claim 1 wherein said processor means comprises an appropriately programmed microprocessor.

9. The computerized flight inspection system according to claim 1 wherein said memory means comprises a parallel-in-serial-out shift register.

10. The computerized flight inspection system according to claim 1 wherein said selected indicia disposed on at least one end of an airport runway comprises two identical indicia disposed on opposite ends of an airport runway.

11. A computerized flight inspection system for providing an accurate reference location with respect to a runway for an aircraft having an inertial navigation system, said flight inspection system comprising:

selected indicia disposed on at least one end of an airport runway;

video scanning means disposed within said aircraft for scanning said selected indicia in a line generally perpendicular to said aircraft'"'"'s line of flight and for generating an output indicative of the scanned video pattern;

inertial navigation means for generating a plurality of signals indicative of aircraft position and attitude;

memory means for storing a reference video pattern;

correlator means coupled to said video scanning means and said memory means for correlating said scanned video pattern and said reference video pattern;

altimeter means for measuring the altitude of said aircraft and for generating a signal indicative thereof; and

processor means coupled to said inertial navigation system, said memory means, said correlator means and said altimeter means for modifying said reference video pattern in response to said plurality of signals indicative of aircraft position and attitude and said altitude signal; and

for generating correction data for said inertial navigation means in response to the altitude and attitude of said aircraft and the output of said correlator means.

12. The computerized flight inspection system according to claim 11 wherein said selected indicia comprises a selected geometric pattern.

13. The computerized flight inspection system according to claim 11 wherein said video scanning means comprises a solid state line scan camera.

14. The computerized flight inspection system according to claim 13 wherein said solid state line scan camera includes a charge couple device line scan image sensor.

15. The computerized flight inspection system according to claim 14 wherein said charge couple device line scan image sensor includes a single row of 1,024 image sensing elements.

16. The computerized flight inspection system according to claim 11 wherein said correlator means comprises a sixty-four bit monolithic digital correlator.

17. The computerized flight inspection system according to claim 11 wherein said altimeter means comprises a laser altimeter.

18. The computerized flight inspection system according to claim 11 wherein said processor means comprises an appropriately programmed microprocessor.

19. The computerized flight inspection system according to claim 11 wherein said memory means comprises a parallel-in-serial-out shift register.

20. The computerized flight inspection system according to claim 11 wherein said selected indicia disposed on at least one end of an airport runway comprises two mirror image indicia disposed on opposite ends of an airport runway.