IP Library › Granted Patent US 10,895,638
Granted Patent B2
US 10,895,638 · App. 15/901,102 · Granted Jan 19, 2021

Radar detection system and radar detection method

Inventors: Shutai Okamura (Osaka, JP); Takeshi Hatakeyama (Osaka, JP); Takahiro Yamaguchi (Osaka, JP); Tsutomu Uenoyama (Osaka, JP)
Assignee: PANASONIC INTELLECTUAL PROPERTY MANAGEMENT CO., LTD.
G01S13/933G01S13/931G06K9/00805G06K9/3241G01S7/003G01S13/934G01S2013/932G01S2013/9316
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,895,638
App. No.
15/901,102
Granted
Jan 19, 2021
Kind
B2
Abstract

A radar detection system according to the present disclosure is a radar detection system that detects an obstacle to an aircraft in an airport. The radar detection system includes a radar apparatus, and a control apparatus. The radar apparatus detects an obstacle by transmitting and receiving a radar signal, and acquires obstacle information regarding the obstacle detected based on the received radar signal. The control apparatus switches the operation of the radar apparatus according to the aircraft state of the aircraft. The control apparatus turns off the radar apparatus when the aircraft takes off, and turns on the radar apparatus when the aircraft makes a landing.

Claims (45)

1. A radar detection system that detects an obstacle to an aircraft in an airport where a first aircraft and a second aircraft take off and make a landing, the radar detection system comprising:

a radar apparatus that is provided in the first aircraft, and is configured to detect an obstacle by transmitting and receiving a radar signal in a three-dimensional range, and acquire obstacle information regarding the obstacle based on the received radar signal, the obstacle information including at least a height of the obstacle;

a first control apparatus that is provided in the first aircraft, includes an airport coordinate system whose origin is set to a predetermined position in the airport, and is configured to calculate a position of the obstacle in the airport coordinate system based on the obstacle information and the airport coordinate system;

a first communication apparatus that is provided in the first aircraft, and is configured to transmit the position of the obstacle in the airport coordinate system;

a second communication apparatus that is provided in the second aircraft, and is configured to receive the position of the obstacle in the airport coordinate system from the first communication apparatus; and

a second control apparatus that is provided in the second aircraft, and is configured to calculate a possibility that the second aircraft will collide with the obstacle based on a position of the second aircraft in the airport coordinate system, and the position of the obstacle in the airport coordinate system.

2. The radar detection system according to claim 1 , wherein

the first control apparatus is configured to change directivity of the radar apparatus based on an aircraft state of the first aircraft.

3. The radar detection system according to claim 2 ,

wherein the first control apparatus is configured to control the directivity to be horizontal, and

the first control apparatus uses a first directivity while the first aircraft is taxiing, and uses a second directivity that is different from the first directivity while the first aircraft is running.

4. The radar detection system according to claim 3 ,

wherein the first control apparatus is configured to use a wide directivity as the first directivity, and uses a narrow directivity as the second directivity.

5. A radar detection system that detects an obstacle to an aircraft in an airport where a control tower is provided, and where a first aircraft and a second aircraft take off and make a landing, the radar detection system comprising:

a radar apparatus that is provided in the first aircraft, and is configured to detect an obstacle by transmitting and receiving a radar signal in a three-dimensional range, and acquire obstacle information regarding the obstacle based on the received radar signal, the obstacle information including at least a height of the obstacle;

a first control apparatus that is provided in the first aircraft, includes an airport coordinate system whose origin is set to a predetermined position in the airport, and is configured to calculate a position of the obstacle in the airport coordinate system based on the obstacle information and the airport coordinate system;

a first communication apparatus that is provided in the first aircraft, and is configured to transmit the position of the obstacle in the airport coordinate system;

a second communication apparatus that is provided in the control tower, and is configured to receive the position of the obstacle in the airport coordinate system from the first communication apparatus, and transmit the position of the obstacle in the airport coordinate system;

a display apparatus that is provided in the control tower, and is configured to display the position of the obstacle in the airport coordinate system;

a third communication apparatus that is provided in the second aircraft, and is configured to receive the position of the obstacle in the airport coordinate system from the second communication apparatus; and

a second control apparatus that is provided in the second aircraft, and is configured to calculate a possibility that the second aircraft will collide with the obstacle based on a position of the second aircraft in the airport coordinate system, and the position of the obstacle in the airport coordinate system.

6. The radar detection system according to claim 5 , wherein

the first control apparatus is configured to change directivity of the radar apparatus based on an aircraft state of the first aircraft.

7. The radar detection system according to claim 6 ,

wherein the first control apparatus is configured to control the directivity to be horizontal, and

the first control apparatus uses a first directivity while the first aircraft is taxiing, and uses a second directivity that is different from the first directivity while the first aircraft is running.

8. The radar detection system according to claim 7 ,

wherein the first control apparatus is configured to use a wide directivity as the first directivity, and uses a narrow directivity as the second directivity.

9. A radar detection method of detecting an obstacle to an aircraft in an airport where a first aircraft and a second aircraft take off and make a landing, the radar detection method comprising:

detecting, by a radar apparatus provided in the first aircraft, an obstacle by transmitting and receiving a radar signal in a three-dimensional range;

acquiring, by the radar apparatus provided in the first aircraft, obstacle information regarding the obstacle based on the received radar signal, the obstacle information including at least a height of the obstacle;

calculating, by a first control apparatus provided in the first aircraft, a position of the obstacle in an airport coordinate system based on the obstacle information and the airport coordinate system, the first control apparatus including the airport coordinate system whose origin is set to a predetermined position in the airport;

transmitting, by a first communication apparatus provided in the first aircraft, the position of the obstacle in the airport coordinate system;

receiving, by a second communication apparatus provided in the second aircraft, the position of the obstacle in the airport coordinate system from the first communication apparatus; and

calculating, by a second control apparatus provided in the second aircraft, a possibility that the second aircraft will collide with the obstacle based on a position of the second aircraft in the airport coordinate system and the position of the obstacle in the airport coordinate system.

10. A radar detection method of detecting an obstacle to an aircraft in an airport where a control tower is provided, and where a first aircraft and a second aircraft take off and make a landing, the radar detection method comprising:

detecting, by a radar apparatus provided in the first aircraft, an obstacle by transmitting and receiving a radar signal in a three-dimensional range;

acquiring, by the radar apparatus provided in the first aircraft, obstacle information regarding the obstacle based on the received radar signal, the obstacle information including at least a height of the obstacle;

calculating, by a first control apparatus provided in the first aircraft, a position of the obstacle in the airport coordinate system based on the obstacle information and an airport coordinate system, the first control apparatus including the airport coordinate system whose origin is set to a predetermined position in the airport;

transmitting, by a first communication apparatus provided in the first aircraft, the position of the obstacle in the airport coordinate system;

receiving, by a second communication apparatus provided in the control tower, the position of the obstacle in the airport coordinate system from the first communication apparatus;

displaying, on a display apparatus provided in the control tower, the position of the obstacle in the airport coordinate system;

transmitting, by the second communication apparatus provided in the control tower, the position of the obstacle in the airport coordinate system;

receiving, by a third communication apparatus provided in the second aircraft, the position of the obstacle in the airport coordinate system from the second communication apparatus; and

calculating, by a second control apparatus provided in the second aircraft, a possibility that the second aircraft will collide with the obstacle based on a position of the second aircraft in the airport coordinate system and the position of the obstacle in the airport coordinate system.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 12, 2018
From: OKAMURA, SHUTAI; HATAKEYAMA, TAKESHI; YAMAGUCHI, TAKAHIRO; UENOYAMA, TSUTOMU
To: PANASONIC INTELLECTUAL PROPERTY MANAGEMENT CO., LTD.
Reel/Frame 045512/0413 →
Continuity (2)
Provisional Application 62557150 · Sep 12, 2017
Related Publication 20190079183A1 · Mar 14, 2019
Cited By (1)
US 12,479,595