Method of autonomous power line detection, avoidance, navigation, and inspection using aerial crafts
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G01V-003/08
B64C-013/18
B64C-013/10
G01S-001/00
G05D-001/00
G01C-023/00
G08G-005/00
출원번호
US-0875927
(2015-10-06)
등록번호
US-9964658
(2018-05-08)
발명자
/ 주소
Hull, David M.
Adelman, Ross N.
출원인 / 주소
The United States of America as represented by the Secretary of the Army
대리인 / 주소
Compton, Eric Brett
인용정보
피인용 횟수 :
0인용 특허 :
17
초록▼
Embodiments of the present invention relate to power line detection, and more particularly, to methods and systems for autonomous power line detection, avoidance, navigation, and inspection. They may be implemented using aerial crafts, but do not have to. According to an embodiment, a method for det
Embodiments of the present invention relate to power line detection, and more particularly, to methods and systems for autonomous power line detection, avoidance, navigation, and inspection. They may be implemented using aerial crafts, but do not have to. According to an embodiment, a method for detecting energized power lines in ambient space in the vicinity of an aerial craft is presented. The method includes measuring, with sensors located on the aerial craft, electric and magnetic fields in the space; and with a power line detection controller, detecting an energized power line in the space in the vicinity of the aerial craft using the sensor data; and determining the orientation of the detected energized power line in the space based on the electric and magnetic field measurements. Similar methods and systems are also presented.
대표청구항▼
1. A method for detecting energized power lines in ambient space in the vicinity of an aerial craft, the method comprising: measuring, with sensors located on the aerial craft, electric and magnetic fields in said space; andwith a power line detection controller, detecting an energized power line in
1. A method for detecting energized power lines in ambient space in the vicinity of an aerial craft, the method comprising: measuring, with sensors located on the aerial craft, electric and magnetic fields in said space; andwith a power line detection controller, detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data;determining the direction of power flow through the energized power line using a Poynting vector, wherein the Poynting vector points parallel to the energized power line; andassociating, as a directional reference, the Poynting vector for the orientation of the detected energized power line in said space. 2. The method of claim 1, wherein detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data comprising: (a) using a derivative of the electric field measurement;(b) using a derivative of the magnetic field measurement; and/or(c) using normalized values of the electric field measurement and/or the magnetic field measurement. 3. The method of claim 2, wherein detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data comprises: (d) using derivatives of both the electric and magnetic field measurements; and/or(e) using normalized derivatives of both the electric and/or magnetic field measurements. 4. The method of claim 1, wherein detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data comprises: (f) using a Poynting vector;(g) using a derivative of the Poynting vector; and/or(h) using a normalized derivative of the Poynting vector. 5. The method of claim 1, wherein detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data further comprises: identifying any power lines in said space based on a determination that the electric field measurement, the magnetic field measurement, a derivative of the electric field measurement, a derivative of the magnetic field measurement, a normalized derivative of the electric field measurement, a normalized derivative of the magnetic field measurement, a Poynting vector, a derivative of the Poynting vector, and/or a normalized derivative of the Poynting vector is/are greater than a corresponding predetermined threshold value for that value. 6. The method of claim 1, further comprises: calculating the Poynting vector using the measured electric and magnetic fields. 7. The method of claim 6, wherein the Poynting vector is calculated every power cycle of the electricity expected to be carried by the power line. 8. The method of claim 1, further comprising: tracking, in said space, the locations of the aerial craft and the associated directional reference for any detected energized power line. 9. The method of claim 1, further comprising: alerting a human pilot to the presence of any detected energized power line in the vicinity of the aerial craft. 10. The method of claim 1, further comprising: automatically controlling the aerial craft to avoid colliding with the energized power line taking into account the associated directional reference for the power line. 11. The method of claim 1, further comprising: controlling the aerial craft to follow along in a direction substantially parallel to the associated directional reference for the detected energized power line. 12. The method of claim 1, wherein detecting an energized power line in said space in the vicinity of the aerial craft using the sensor data comprises: using a derivative of the Poynting vector. 13. A system for detecting energized power lines in ambient space in the vicinity of an aerial craft, the system comprising: electric field and magnetic field sensors located on the aerial craft configured to measure the electric and magnetic fields in said space; anda power line detection controller configured to: detect an energized power line in said space in the vicinity of the aerial craft using the sensor data;determine the direction of power flow through the energized power line using a Poynting vector, wherein the Poynting vector points parallel to the energized power line; andassociate, as a directional reference, the Poynting vector for the orientation of the detected energized power line in said space. 14. The system of claim 13, wherein the electric field sensor and magnetic field sensor each comprise a single three-axis sensor or three single-axis sensors aligned orthogonally. 15. The system of claim 13, wherein the electric field sensor and magnetic field sensor are located at the same position on the aerial craft. 16. The system of claim 13, wherein there is a pair of electric field and magnetic field sensors, and the controller is further configured to take derivative measurements from said sensors. 17. The system of claim 13, further comprising: an instrument panel having audio means, visual means, or both, for alerting a pilot to a detected energized power line; and means for displaying the location and/or orientation of the power lines to the pilot. 18. The system of claim 13, further comprising a dynamic flight controller, wherein the power line detection controller is further configured to determining maneuvers for the aerial craft to avoid the detected energized power lines which are provided to the dynamic flight controller taking into account the associated directional reference for the power line. 19. The system of claim 18, wherein the power line detection controller is further configured to determine maneuvers for the aerial craft to inspect the detected energized power lines taking into account the associated directional reference for the power line. 20. The system of claim 13, wherein the power line detection controller is located on the aerial craft. 21. An aerial craft configured to detect energized power lines in ambient space comprising: electric field and magnetic field sensors configured to measure the electric and magnetic fields in said space in the vicinity of the aerial craft; anda power line detection controller configured to: detect an energized power line in said space in the vicinity of the aerial craft using the sensor data;determine the direction of power flow through the energized power line using a Poynting vector, wherein the Poynting vector points parallel to the energized power line; andassociate, as a directional reference, the Poynting vector for the orientation of the detected energized power line in said space. 22. A device configured to detect energized power lines comprising: electric field and magnetic field sensors configured to measure the electric and magnetic fields in said space; anda controller configured to: detect an energized power line in said space using the sensor data,wherein, in detecting an energized power line in said space in the vicinity of device using the sensor data, the controller is configured to:(a) use a derivative of the electric field measurement;(b) use a derivative of the magnetic field measurement;(c) use a normalized derivative of the electric field measurement;(d) use a normalized derivative of the magnetic field measurement;(e) use a derivative of the Poynting vector; and/or(f) use a normalized derivative of the Poynting vector. 23. The device of claim 22, wherein the device is hand-held or incorporated into a helmet or vehicle.
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이 특허에 인용된 특허 (17)
Waite, James W.; Gudmundsson, Thorkell; Gargov, Dimitar, Autonomous vehicle power line position and load parameter estimation.
Simons,David J.; Carrigan,Charles R.; Harben,Philip E.; Kirkendall,Barry A.; Schultz,Craig A., Poynting-vector based method for determining the bearing and location of electromagnetic sources.
Merritt William E. (1431 SE. Knight Portland OR 97202) Johnson Joel (Lake Oswego OR), System for warning aircraft pilot of potential impact with a power line and generating time-to-time impact signal.
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