Correlation system for multiple-sensor reconnaissance vehicle

• US 4,122,521 A
• Filed: 04/13/1977
• Issued: 10/24/1978
• Est. Priority Date: 10/20/1975
• Status: Expired due to Term

• Current Assignee: Northrop Corporation
• Original Assignee: Northrop Corporation
• Inventors: Tracy, Robert E., Rick, Horst, Olsen, Lowell V., Keppel, Richard A., Mitchell, Harvey A., Colas, James K.
• Primary Examiner(s): Ruggiero, Joseph F.
• Application Number:
  US05/787,270
• Time in Patent Office: 559 Days
• Field of Search: 235/150.2, 235/150.26, 235/150.27, 343/5 CM, 343/5 DP, 343/5 PC, 343/6 A, 343/6 TV, 343/112 C, 33/1 A, 33/18 C, 354/21, 354/65, 354/66, 354/68, 354/69, 354/71, 354/72, 354/73, 354/75, 178/15, 358/109, 358/139, 358/903, 358/130, 358/131, 358/132, 364/424, 364/443, 364/444, 364/449, 364/456, 364/514, 364/516
• US Class Current: 701/200
• CPC Class Codes: G01S 7/04 Display arrangements

Abstract

A plurality of sensors of various types each initiating a marker signal as it produces a "frame" of information sensed, such as a camera film frame for example. A computer in the navigation system of the reconnaissance craft receives the marker signals and generates respective successive frame count numbers which are fed back to the proper respective sensors and recorded directly on the individual frames to whch they pertain while the frames are still being taken or sensed by the sensors. At essentially the same time as the frame count number is being processed, the computer outputs a block of information to be stored and recorded for that one frame (sensor product), this information including the identifying frame count number, the sensor which took it, the time of occurrence, and the geographical location of the event as provided by the navigation system. Thus, each frame of intelligence gathered and later processed on the ground is simply correlated with the recorded block of desired data concerning it by a ground interpreter. An additional feature is a process of including photographic and location data of certain known ground sites during the same reconnaissance flight, providing a comparison capability to enable correction of any nagivation system biases and thereby obtain very precise geographic coordinate location of the sensor products.

Claims

1. A multiple-sensor reconnaissance system for an aircraft having a navigation system and a digital computer therein, said computer continually carrying present navigation parameters from said navigation system, comprising:

a. a plurality of sensors each capable of making frames of intelligence according to the type of energy sensed thereby;

b. first trigger means in each of said sensors for generating and passing a marker signal to said computer each time a sensor frame of information is to be taken;

c. means in said computer responsive to each said marker signal for identifying the sensor, producing a new respective frame count number and sending said number back to the originating sensor;

d. number recording means in each sensor for indicating said frame count number on said intelligence frame corresponding to the said marker signal;

e. information collecting means in said computer for producing a block of digital information signals containing said frame count number, sensor identification and existing navigation parameters from said navigation system including geographical location of said aircraft; and

f. information recording means for recording said computer-produced information signals essentially simultaneously with each time a marker signal is sent to said computer.

2. Apparatus in accordance with claim 1 wherein each of said sensors comprises an individual on-off control means, a holding register for receiving said frame count number from said computer, and second trigger means mechanically operated by said sensor to enter said frame count number at the desired time directly onto its associated frame.

3. Apparatus in accordance with claim 1 wherein one or more of said sensors comprises a photographic camera, frame count number display means for displaying successively said numbers supplied from said computer, means for optically exposing each said displayed number onto the film in said camera, and second trigger means for timing the number display exposure on said film once each frame period.

4. Apparatus in accordance with claim 1 wherein one or more of said sensors comprises a magnetic recording device including a recording medium, means for applying the successive frame count numbers received from said computer onto said medium when triggered, and second trigger means for applying respectively said successive numbers once each frame period.

5. Apparatus in accordance with claim 1 wherein one or more of said sensors comprises a radar device including a cathode ray tube, a camera for photographing the face of said tube, means for exposing the film of said camera to a display of the respective frame count numbers provided by said computer, and second trigger means for providing said display once each camera frame period.

6. Apparatus in accordance with claim 1 wherein said sensor identification means comprises selector logic for providing a parallel format multiple-line binary coded output from said computer, and gating means for passing said frame count number to only the selected sensor.

7. Apparatus in accordance with claim 1 wherein said frame count number-producing means comprises means for generating a multiple-bit serial pulse code output from said computer representing said number, and means for adding a numerical "one" to the frame count number of a sensor each time a marker signal is received therefrom.

8. In a multiple-sensor reconnaissance system for an aircraft having a navigation system and a digital computer, said computer continually carrying present navigation parameters from said navigation system;

the method of correlating the products of the sensors, comprising;

a. designating a discrete portion of sensor intelligence gathered as a frame;

b. generating a marker signal for each frame to be made by each sensor;

c. assigning a frame count number in consecutive order to identify each frame from said sensors in response to each marker signal;

d. producing a sensor identification signal from each said marker signal;

e. supplying each said frame count number to the respective said sensor from which the corresponding marker signal came;

f. indicating each said frame count number in readable form directly on said sensor frame to which it applies; and

g. substantially simultaneously recording a line of information containing the identifying frame count number, its sensor number, and existing navigation parameters from said navigation system including geographical location of said aircraft;

whereby

h. each sensor frame can be quickly paired with the recorded information line giving its geographical location and other data.

9. Method in accordance with claim 8 wherein said information lines are magnetically recorded, and including printing a listing of said recorded information for ground comparison with subsequently processed sensor frames.

10. In a correlation system for the sensor product data of an airborne reconnaissance system including a navigation system;

the method of obtaining precise geographical locations of the frames of sensor data gathered during a flight, comprising;

a. recording data concerning each sensor frame made, said data including identification of the particular sensor frame and the existing coordinate location of the aircraft at the exact time said frame was made according to the information from said navigation system;

b. flying over and photographing two substantially spaced ground points whose coordinate locations are known beforehand, and recording the same data for said points the same as for all the other sensor frames made;

c. subsequently comparing the said recorded data for said two points with the said known locations to determine the coordinate location differences; and

d. applying computed correction factors derived from said differences to all other said sensor frame location data recorded;

whereby

e. whatever inaccuracy and bias of said navigation system exists is removed from the final results.