Radar apparatus

• US 6,067,048 A
• Filed: 02/11/1999
• Issued: 05/23/2000
• Est. Priority Date: 02/12/1998
• Status: Expired due to Term

• Current Assignee: Toyota Jidosha Kabushiki Kaisha (Toyota Motor Corporation)
• Original Assignee: Toyota Jidosha Kabushiki Kaisha (Toyota Motor Corporation)
• Inventors: Yamada, Yukinori
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Phan, Dao L.
• Application Number:
  US09/247,854
• Time in Patent Office: 467 Days
• Field of Search: 342/5, 342/25, 342/81, 342/39, 342/382, 342/379, 342/368
• US Class Current: 342/382
• CPC Class Codes: G01S 13/345 using triangular modulation
• CPC Class Codes: G01S 13/426 Scanning radar, e.g. 3D radar G01S13/66 takes precedence
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H01Q 3/24 varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching

Abstract

The object of the invention is to suppress relative power of grating lobes in electronic scanning radar apparatus. This radar apparatus is a radar apparatus comprising a transmitting antenna and a receiving antenna, the receiving antenna being an array antenna having a plurality of antenna elements, the radar apparatus being adapted to effect electronic scanning of an antenna beam of the receiving antenna, wherein each of the plurality of antenna elements is comprised of a plurality of elemental antennas, so as to have a predetermined directional pattern, and wherein a synthetic pattern of the directional pattern of each antenna element and a directional pattern of the transmitting antenna has a depressed shape of relative power at an angle where a grating lobe of the receiving antenna appears.

Claims

1. A radar apparatus comprising a transmitting antenna and a receiving antenna, said receiving antenna being an array antenna having a plurality of antenna elements, said radar apparatus being adapted for carrying out the forming and scanning of an antenna beam of said receiving antenna according to a digital beamforming operation, and each of said plurality of antenna elements being comprised of a plurality of elemental antennas so as to have a predetermined directional pattern,

wherein a synthetic pattern of the directional pattern of each of said antenna elements and a directional pattern of said transmitting antenna has a depressed shape of relative power at an angle where a grating lobe of said receiving antenna appears, and said forming and scanning of the antenna beam of said receiving antenna is carried out under the assumption that each of said antenna elements has a non-directional pattern, and a directional angle of a main beam is obtained by correcting an angle of the main beam computed under said assumption with a correction value previously determined according to the computed angle.

2. The radar apparatus according to claim 1, wherein said transmitting antenna is comprised of a plurality of elemental antennas.

3. An electronic scanning method for use in a radar apparatus comprising:

transmitting a transmit signal from a transmitting antenna;

receiving a receive signal in a receiving antenna, said receiving antenna being an array antenna having a plurality of antenna elements, each of said plurality of antenna elements being comprised of a plurality of elemental antennas so as to have a predetermined directional pattern, wherein a synthetic pattern of the directional pattern of each of said antenna elements and a directional pattern of said transmitting antenna has a depressed shape of relative power at an angle where a grating lobe of said receiving antenna appears;

scanning an antenna beam of said receiving antenna according to a digital beamforming operation under the assumption that each of said antenna elements has a non-directional pattern;

computing an angle of a main beam under said assumption; and

determining a directional angle of the main beam by correcting the computed angle using a correction value previously determined according to the computed angle.