Seeker head particularly for automatic target tracking

• US 5,702,068 A
• Filed: 09/25/1979
• Issued: 12/30/1997
• Est. Priority Date: 09/26/1978
• Status: Expired due to Term

• Current Assignee: Bodenseewerk Gerätetechnik Gmbh
• Original Assignee: Bodenseewerk Gerätetechnik Gmbh
• Inventors: Tessari, Hans, Stoll, Alfred, Eckhardt, Reiner, Gulitz, Wolfgang
• Primary Examiner(s): Jordan, Charles T.
• Application Number:
  US06/079,479
• Time in Patent Office: 6,671 Days
• Field of Search: 244/3.16, 244/3.15, 244/3.19
• US Class Current: 244/3.16
• CPC Class Codes: F41G 7/2213 maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves

Abstract

In a seeker head a field of view is scanned cyclically for providing picture informations referenced to a seeker-fixed coordinate system. The seeker carries a gyro assembly, which provides attitude variation signals as a function of attitude variations of the seeker relative to inertial space. The attitude variation signals are applied to a coordinate transformer which transforms all picture informations with their addresses into an inertial coordinate system which coincided with the seeker-fixed coordinate system after the completion of the preceding scan. Thereby during each scan all picture informations are transformed into one single inertial coordinate system. After the completion of the scan, the picture informations are again transformed into an inertial coordinate system, which coincided with the seeker-fixed coordinate system at the end of said scan, and are stored in a memory. This is the same coordinate system into which the picture informations will be transformed during the next-following scan. Thus at the end of this next-following scan the picture informations from two consecutive scans are available, which are referenced to one single, common coordinate system and are therefore comparable in spite of attitude variations of the seeker. These picture informations are applied to signal processing means, such as a target selection logic.

Claims

1. A system comprising:

(a) a carrier,

(b) a seeker head movably mounted on the carrier to "look" towards a target,

(c) field of view scanning means associated with the seeker head for periodically scanning a field of view observed by the seeker head,

(d) a gyro assembly associated with the seeker head,

(e) image storing means for storing the results of scans, and

(f) a coordinate transformer circuit receiving signals generated by the gyro assembly and controlled thereby to reference and compare the images of two consecutive scans to a common coordinate system.

2. The system as set forth in claim 1, characterized in that the gyro assembly comprises rate gyros, from the signals of which the attitude variation signals are generated by means of a coordinate transformer and integrator circuit, the integrators of the coordinate transformer and integrator circuit being arranged to be reset to zero once during each scan.

3. The system as set forth in claim 1, characterized in

that the gyro assembly comprises pitch, yaw and roll gyros which respond to angular speeds about the pitch, yaw and roll axes, respectively,

that the output signal of the roll gyro is applied to a first integrator the output signal of which is converted by a first analog-to-digital converter into a digital attitude variation signal representing the roll movement of the seeker head,

that the analog output signal of the first integrator is applied to a sine function generator and to a cosine function generator,

that the output signals of the sine function generator, of the cosine function generator, of the pitch and of the yaw gyros are applied to a first computing circuit which forms therefrom an output signal

4. The system as set forth in claim 1, characterized in that the gyro assembly comprises pitch, yaw and roll gyros which respond to the angular speeds about the pitch, yaw and roll axes, respectively,

that the output signal of the roll gyro is applied to a first integrator the output signal of which is converted by a first analog-to-digital converter into a digital attitude deviation signal representing the roll movement of the seeker head

that the analog output signal of the first integrator and the output signals of the pitch and of the yaw gyros are applied to a first computer circuit, which forms an output signal

5. The system as set forth in claim 3 or 4, characterized in that the coordinate transformer circuit (100) comprises a first digital computer (258) to which the output signal (φ

) of the first analog-to-digital converter and coordinates (Y_A,Z_A) of a picture element in the seeker head-fixed coordinate system are applied, and which forms

space="preserve" listing-type="equation">Y.sub.A cos φ

-Z.sub.A sin φ

,

wherein Y_A and Z_A are the coordinates of the picture elements in the seeker head-fixed coordinate system and φ

is the output signal of the first analog-to-digital converter,

that, furthermore, the coordinate transformer circuit (100) comprises a first adder (260) to which the digital output signal of the first computer and the output signal (Y_o) of the second analog-to-digital converter are supplied and which provides a corrected coordinate (Y_K) in an inertial coordinate system,

that the coordinate transformer circuit (100) comprises a second digital computer (264) to which the output signal (φ

) of the first analog-to-digital converter and the coordinates (Y_A,Z_A) of the picture element in the seeker head-fixed coordinate system are applied, and which forms

space="preserve" listing-type="equation">Y.sub.A sinφ

+Z.sub.A cos φ

,

and

that, eventually, the coordinate transformer circuit (100) comprises a second adder (266) to which the digital output signal of the second computer (264) and the output signal (Z_o) of the third analog-to-digital converter are applied and which provides the other corrected coordinate (Z_K) in the inertial coordinate system.

6. The system as set forth in claim 5, characterized in that each of the computers (258,264) comprises a pair of read-only memories (268,270), each of which has applied thereto as address a respective one of the coordinates (Y_A and Z_A) in the seeker head-fixed coordinate system, each in combination with the output signal (φ

) of the first analog-to-digital converter, the read-only memories having stored under each address Y_A cos φ and

-Z_A sin φ

or Y_A sin φ and

Z_A cos φ

, respectively, and that the outputs of the read-only memories (268,270) are appied to an adder (272).

7. The system as set forth in anyone of the claim 1, characterized in

that, during each signal processing cycle in a first operation during a scan, the picture informations are transformed by the coordinate transformation circuit into an inertial coordinate system which after completion of the preceding scan, coincided with the seeker head-fixed coordinate system, and the picture informations thus transformed with respect to their addresses are written into a first memory,

that upon completion of each scan the attitude variation signals from the coordinate transformation and integrator circuit (84) are written into an end value memory (94),

that in a second operation the picture informations stored in the first memory (102) are transformed by the coordinate transformer circuit (100), with the end values of the attitude variation signals stored in the end value memory (94), into an inertial coordinate system which, at the end of the scan, coincided with the seeker head-fixed coordinate system, and the picture informations thus transformed with respect to their addresses are written into a second memory (104), and

that a target selection logic (106) is provided, to which the data from the first and second memories (102 and 104, respectively) are applied.

8. The system as set forth in claim 7, characterized in

that, by a signal (TA) provided by the target selection logic (106) upon the target data provided by the target selection logic (106) are transformed by the coordinate transformation circuit (100) with the end values (Y_E,Z_E, φ

_E) of the attitude variation signals provided by the end value memory, into an inertial coordinate system which coincided with the seeker head-fixed coordinate system at the end of the last scan, and

that the target data thus transformed are written into a deviation memory, which applies deviation signals to the controller (60).