Method for navigating an aerial drone in the presence of an intruding aircraft, and drone for implementing said method
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G08G-005/00
G08G-005/04
출원번호
US-0310015
(2015-04-30)
등록번호
US-10157547
(2018-12-18)
우선권정보
FR-14 54215 (2014-05-12)
국제출원번호
PCT/EP2015/059603
(2015-04-30)
국제공개번호
WO2015/173033
(2015-11-19)
발명자
/ 주소
Farjon, Julien
출원인 / 주소
SAGEM DEFENSE SECURITE
대리인 / 주소
Muncy, Geissler, Olds & Lowe, P.C.
인용정보
피인용 횟수 :
0인용 특허 :
1
초록▼
A method of navigation of an aerial drone in the presence of at least one intruding aircraft in an airspace zone surrounding the drone, wherein an estimated distance between the drone and the intruding aircraft is calculated based on a strength of the signal received and validated if an estimated va
A method of navigation of an aerial drone in the presence of at least one intruding aircraft in an airspace zone surrounding the drone, wherein an estimated distance between the drone and the intruding aircraft is calculated based on a strength of the signal received and validated if an estimated value of an element of positioning data calculated by the drone using the estimated distance substantially corresponds to a measured value of the element of positioning data. An aerial drone designed for implementation of this method.
대표청구항▼
1. A method of navigation of an aerial drone in the presence of at least one intruding aircraft in an airspace zone surrounding the drone, characterised in that the method comprises the stages, implemented via a piloting device, mounted on the drone, involving: receiving via the piloting device, mou
1. A method of navigation of an aerial drone in the presence of at least one intruding aircraft in an airspace zone surrounding the drone, characterised in that the method comprises the stages, implemented via a piloting device, mounted on the drone, involving: receiving via the piloting device, mounted on the drone a signal from the intruding aircraft, which signal comprises at least the altitude of the intruding aircraft and calculating an estimated distance between the drone and the intruding aircraft based on a strength of the received signal;capturing via an optronic device associated with the piloting device, at least one image of the intruding aircraft and determining a bearing angle of the intruding aircraft based on this image;extracting from the signal the altitude transmitted by the intruding aircraft;calculating, using the estimated distance, an estimated value of an element of positioning data of the intruding aircraft or the drone;comparing the estimated value of the element of positioning data with a measured value of the element of positioning data and taking account of the distance calculated for navigation if the estimated value substantially matches the measured value; andcommanding the aerial drone using the calculated distance. 2. The method according to claim 1, wherein the element of positioning data is the altitude of the intruding aircraft, said method therefore comprising the stages of: calculating an estimated altitude of the intruding aircraft based on the bearing angle and the estimated distance;comparing the estimated altitude with the transmitted altitude and taking account of the estimated distance for navigation if the estimated altitude substantially matches the transmitted altitude. 3. The method according to claim 1, wherein the element of positioning data is the bearing angle of the intruding aircraft, said method therefore comprising the stages of: calculating an estimated bearing angle of the intruding aircraft based on the altitude of the drone, the transmitted altitude and the estimated distance;comparing the estimated bearing angle with the bearing angle determined based on the image and taking account of the estimated distance for navigation if the estimated bearing angle substantially matches the bearing angle determined based on the image. 4. The method according to claim 1, comprising the subsequent stage of calculating at least one closing speed of the drone and of the intruding aircraft and an estimated time to collision based on the estimated distance calculated on two successive images. 5. The method according to claim 4, comprising the stages of calculating a closing speed of the drone and of the intruding aircraft based on a dimension of the intruding aircraft in two successive images and comparing the closing speed determined based on a dimension of the intruding aircraft in two successive images and the closing speed determined based on the estimated distance calculated in two successive images. 6. An aerial drone comprising a piloting device including a data processing unit connected to an altitude measuring instrument, to an optronic detection device designed to determine a bearing angle of an intruding aircraft operating in an area surrounding the drone and to a receiver for receiving a signal that is emitted by the intruding aircraft and which includes an altitude of the intruding aircraft, wherein the piloting device is designed to: calculate an estimated distance between the drone and the intruding aircraft based on a strength of a signal received by the receiver;capture at least one image of the intruding aircraft by the optronic device and determine the bearing angle of the intruding aircraft based on this image;extract from the signal the altitude transmitted by the intruding aircraft;calculate, using the estimated distance, an estimated value of an element of positioning data of the intruding aircraft or the drone;compare the estimated value of the element of positioning data with a measured value of the element of positioning data and taking account of the distance calculated for navigation if the estimated value substantially matches the measured value; andcommand the aerial drone using the calculated distance. 7. The drone according to claim 6, comprising an interrogator designed to interrogate a transponder of the intruding aircraft. 8. The drone according to claim 6, wherein the data processing unit comprises a device for means of estimating a closing speed of the intruding aircraft. 9. The drone according to claim 8, wherein the device for estimating is an image processing unit designed to determine the closing speed of the intruding aircraft as a function of a size of the intruding aircraft in two successive images captured by the optronic device. 10. The drone according to claim 8, wherein the device for estimating comprises a Kalman filter for calculating the closing speed based on the estimated distances. 11. The drone according to claim 10, wherein the Kalman filter is designed to provide periodically estimated distances and closing speeds based on the images provided by the optronic device and the altitude transmitted by the aircraft. 12. The drone according to claim 11, wherein the estimated distances and the closing speeds are associated with an identifier of the intruding aircraft, said identifier being extracted from the signal received by drone transponder. 13. The drone according to claim 6, wherein the receiver comprises a directional antenna. 14. The drone according to claim 6, wherein the element of positioning data is the altitude transmitted by the intruding aircraft. 15. The drone according to claim 6, wherein the element of positioning data is the bearing angle of the intruding aircraft.
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이 특허에 인용된 특허 (1)
Khvilivitzky Alexander (9127 NW. 43 Ct. Coral Springs FL 33065), Visual collision avoidance system for unmanned aerial vehicles.
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