High repetition frequency side-looking pulse radar system

• US 4,064,510 A
• Filed: 06/18/1976
• Issued: 12/20/1977
• Est. Priority Date: 06/24/1975
• Status: Expired due to Term

• Current Assignee: Thomson-CSF (Thales SA)
• Original Assignee: Thomson-CSF (Thales SA)
• Inventors: Chabah, Maurice
• Primary Examiner(s): Hubler, Malcolm F.
• Application Number:
  US05/697,738
• Time in Patent Office: 550 Days
• Field of Search: 343/5 CM, 343/7.5, 343/16 M
• US Class Current: 342/88
• CPC Class Codes: G01S 13/9092 combined with monopulse techniques

Abstract

The invention relates to side-looking radar systems and more especially to high altitude airborne radar systems functioning at a high repetition frequency. In order to avoid ambiguities in regard to distance, the antenna comprises an additional channel which has a radiation pattern which has an odd symmetry about its axis and means are connected to said antenna for deriving the angular interval relative to the axis of the antenna of the direction of the obstacle corresponding to the received echoes. Gating means select the angular interval signal at the middle of the recurrence, for controlling the recurrence frequency of the radar and maintaining the ambiguous areas outside the selected observed area.

Claims

1. In a side-looking airborne pulse radar system, means for maintaining the direction of an echo received in the middle of each recurrence from a ground area observed by the radar system, substantially coincident with a predetermined axis, comprising:

angular measuring means responsive to the angular interval between said axis and the direction of received ground echos and to the pulse repetition frequency of the radar system for providing an output signal indicative of the amplitude and the sense of the angular inerval between said axis and the direction of the echo received in the middle of each recurrence; and

frequency controlled pulse repetition frequency generator means coupled to the output of said angular measuring means for controlling the pulse repetition frequency of said radar system so as to tend to reduce said angular interval to null.

2. A radar system as claimed in claim 1, wherein said angular measuring means comprises:

antenna means having a radiation pattern which has an odd symmetry about said predetermined axis in a vertical plane;

receiving means coupled to said antenna means for providing echo signals repesentative of the magnitude and the sense of the angular interval between said predetermined axis and the direction of obstacles on the ground corresponding to said echo signals; and

gating means coupled to an output of said receiving means and to said frequency controlled pulse repetition frequency generator means for selecting the only echo signal received in the middle of the recurrence of the radar system.

3. A radar system as claimed in claim 2, wherein said antenna means comprises a sum channel having a radiation pattern which has an even symmetry about said predetermined axis for providing a sum signal Σ

and a difference channel having a radiation pattern which has an odd symmetry about said predetermined axis for providing a difference signal Δ

, and wherein said receiving means comprises a combination circuit connected to said sum channel and said difference channel of said antenna for providing output signals Σ

+ jΔ and

Σ

- jΔ

, a phase-detector circuit having two inputs and an output for delivering the angular echo signals and two limiting circuits respectively connected between the outputs of the combination circuit and the inputs of said phase-detector circuit.

4. A radar system as claimed in claim 1, wherein said frequency controlled pulse repetition frequency generator means comprise a controllable frequency oscillator having a control input, a synchronization circuit connected to said oscillator for delivering control pulses alternately to the radar system for controlling the pulse repetition thereby on the one hand and to the angular measuring means on the other hand, and amplifying and filtering means connected to said control input of said oscilator for receiving output signal from the angular measuring means and controlling thereby the frequency of said oscillator.