Radar system

• US 4,656,479 A
• Filed: 01/14/1985
• Issued: 04/07/1987
• Est. Priority Date: 02/08/1984
• Status: Expired due to Term

• Current Assignee: Mitsubishi Denki Kabushiki Kaisha (Mitsubishi Electric Corporation)
• Original Assignee: Mitsubishi Denki Kabushiki Kaisha (Mitsubishi Electric Corporation)
• Inventors: Fujisaka, Takahiko, Kirimoto, Tetsuo, Kondo, Michimasa
• Primary Examiner(s): Tubbesing, T. H.
• Assistant Examiner(s): Hellner, Mark
• Application Number:
  US06/690,938
• Time in Patent Office: 813 Days
• Field of Search: 343/16 R, 343/5 FT, 343/422-424, 343/444, 343/6.5 R, 343/16 M, 342/94
• US Class Current: 342/94
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 13/76 wherein pulse-type signals are transmitted

Abstract

A radar system for finding the location of a second flying object from a first flying object, comprises a nondirectional antenna for radiating a first radio wave from the first flying object, a second nondirectional antenna provided on the second flying object to receive the first radio wave and to radiate a second radio wave generated by modulating the received first radio wave and an array antenna provided on the first flying object to receive the second radio wave. The respective amplitudes of the signals given by the antenna elements of the array antenna are compared individually with a specified level and an operation for determining the direction of arrival of the second radio wave is executed using the signals given by all the antenna elements when either of the amplitudes of the signals given by the antenna elements is greater than the specified level.

Claims

1. A radar system comprising:

a radio wave transmitting means having a transmitter which generates a first radio wave, and a first nondirectional antenna which radiates the first radio wave generated by the transmitter into external space, said radio wave transmitting means being aboard a first flying object;

a radio wave transmitting and receiving means having a second nondirectional antenna for receiving the first radio wave radiated by the first nondirectional antenna, and a transponder which amplifies and modulates the first radio wave received through the second nondirectional antenna to generate a second radio wave and to radiate the second radio wave through the second nondirectional antenna into the external space, said radio wave transmitting and receiving means being aboard a second flying object; and

a radio wave receiving means having an array antenna having a two-dimensional arrangement of a plurality of nondirectional antenna elements which receive the second radio wave generated by the transponder, a plurality of receivers which amplify and detect the second radio wave received through the nondirectional antenna elements constituting the array antenna to generate a plurality of corresponding receiving signals, means to decide whether or not the amplitude of the receiving signal detected by a designated one of the receivers is greater than a specified threshold, means to generate a trigger pulse only when the amplitude detected by the designated receiver exceeds the specified threshold, a plurality of sampling and quantizing means which, in response to the trigger pulse, sample and quantize simultaneously the plurality of receiving signals generated by the receivers, and a goniometric means which processes the output signal of the sampling and quantizing means to measure the direction of arrival of the second radio wave, and said radio wave receiving means being aboard said first flying object.

2. A radar system as set forth in claim 1, wherein said transmitter for generating the first radio wave includes means to encode the first radio wave and said transponder includes means to decode the coded first radio wave and means to control the transmission of the second radio wave in accordance with the code.

3. A radar system as set forth in claim 1 wherein one of the nondirectional antenna elements constituting the array antenna is used in common both as one antenna element of the array antenna and as the first nondirectional antenna for transmitting the first radio wave.

4. A radar system as set forth in claim 1, wherein said goniometric means includes Fourier transformers for providing discrete Fourier transformation, means for providing monopulse operation, and peak detectors for detecting maximum values.

5. A radar system aboard a flying object, comprising:

a nondirectional transmitting antenna, a transmitter for energizing the nondirectional transmitting antenna to radiate a radio wave into external space;

an array antenna having a two-dimensional arrangement of a plurality of nondirectional antenna elements which receive the reflection of the radio wave radiated by the nondirectional antenna and reflected by a target;

a plurality of receivers which amplify and detect said reflection received by the corresponding antenna elements of the array antenna to produce a plurality of corresponding receiving signals;

means for determing and amplitude of the receiving signal detected by one of said receivers being greater than a specified threshold to generate a sampling pulse;

a plurality of sampling and quantizing means operated by the sampling pulse for sampling and quantizing the plurality of receiving signals produced by said receivers simultaneously; and

means for determining the direction of arrival of said reflection from the output signals of said sampling and quantizing means.

6. A radar system as set forth in claim 5, wherein one of the nondirectional antenna elements of said array antenna is used in common as one antenna element of the array antenna and as the nondirectional transmitting antenna.

7. A radar system as set forth in claim 6, wherein said direction of arrival determining means includes Fourier transformers for providing discrete Fourier transformation, means for providing monopulse operation, and peak detectors for detecting maximum values.