Method for acquiring images from arbitrary perspectives with UAVs equipped with fixed imagers
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H04N-007/18
B64D-047/08
G05D-001/00
출원번호
US-0233290
(2012-06-21)
등록번호
US-9641810
(2017-05-02)
우선권정보
EP-11170993 (2011-06-22)
국제출원번호
PCT/EP2012/061928
(2012-06-21)
§371/§102 date
20140116
(20140116)
국제공개번호
WO2012/175592
(2012-12-27)
발명자
/ 주소
Zufferey, Jean-Christophe
Beyeler, Antoine
출원인 / 주소
SENSEFLY S.A.
대리인 / 주소
DLA Piper LLP (US)
인용정보
피인용 횟수 :
1인용 특허 :
2
초록▼
A method for acquiring images of a photographic target from arbitrary perspectives with an unmanned aerial vehicle (UAV) equipped with at least one image acquisition device having a fixed acquisition direction with respect to the vehicle, said UAV having automatic navigation means allowing to reach
A method for acquiring images of a photographic target from arbitrary perspectives with an unmanned aerial vehicle (UAV) equipped with at least one image acquisition device having a fixed acquisition direction with respect to the vehicle, said UAV having automatic navigation means allowing to reach an arbitrary location and automatic attitude control means allowing to transiently reach an arbitrary orientation in space, said photographic target being outside the current field of view of the acquisition device while the UAV flies along a predefined flying path, this method comprising: computing a target UAV position and an orientation in space required to acquire a desired image from a set of parameters, navigating to said target UAV position, modifying an attitude of the UAV in order to modify the acquisition direction to point toward the photographic target, acquiring images, and starting a recovery phase by controlling the UAV back to cruise attitude and navigate back along the predefined flying path.
대표청구항▼
1. A method for acquiring images of a photographic target from arbitrary perspectives with an unmanned aerial vehicle (UAV) equipped with at least one image acquisition device having a fixed acquisition direction with respect to the vehicle, said UAV having an automatic navigation system that allows
1. A method for acquiring images of a photographic target from arbitrary perspectives with an unmanned aerial vehicle (UAV) equipped with at least one image acquisition device having a fixed acquisition direction with respect to the vehicle, said UAV having an automatic navigation system that allows the UAV to reach an arbitrary location and automatic attitude control system that allows the UAV to transiently reach an arbitrary orientation in space, said photographic target being outside a current field of view of the acquisition device while the UAV flies along a predefined flying path, the method comprising the steps of: computing a target UAV position and an orientation in space required to acquire a desired slanted image from a set of parameters pertaining to the desired photographic target, a desired perspective and a relative orientation of the image acquisition device with respect to the UAV;determining an anticipatory location at a target UAV altitude and spaced apart from the target UAV position at a distance determined by one or more flight dynamics of the UAV, the anticipatory location being on a line between the target UAV position and the photographic target; andnavigating, using the automatic navigation system, to said anticipatory location before navigating to the target UAV position;navigating, after reaching the anticipatory location, using the automatic navigation system, to said target UAV position;modifying an attitude, which comprises modifying at least one of a pitch or roll of the UAV in order to modify the acquisition direction to point toward the photographic target, thereby deviating from the predefined flying path into a transient phase of flight;acquiring images during the transient phase of flight when the acquisition direction points toward the photographic target with the desired perspective; andstarting a recovery phase by controlling the UAV back to the predefined flying path. 2. The method according to claim 1, further comprising the step of determining, a direction and an amplitude of a wind and shifting the anticipatory location laterally such that to compensate for a lateral drift of the wind. 3. The method according to claim 1, further comprising the steps of: calculating a new altitude resulting from modifying a current attitude of the UAV; andshifting the anticipatory location vertically to compensate for the new altitude. 4. The method according to claim 1, further comprising the steps of: deploying a retractable objective of the image acquisition device while the UAV is in the air or when the UAV reaches the target position; andretracting the retractable objective after the image acquisition device has finished acquiring the images or before landing. 5. The method according to claim 1, wherein the image acquisition device comprises an objective with zoom capabilities, the method further comprising the step of: taking into account the zoom factor to determine the target position. 6. The method according to claim 1, wherein the UAV comprises a plurality of image acquisition devices arranged on its airframe, each acquiring device taking images in sequence. 7. The method according to claim 1, wherein the UAV is powered by a propulsion motor during the navigation, the method further comprising the step of reducing a speed of the UAV or stopping said motor when acquiring the images. 8. The method according to claim 1, wherein the computing of the target UAV position comprises the steps of: determining, on a map display, a ground coverage trapeze defining a desired image and perspective by means of virtual handles allowing to change the trapeze position, shape and orientation; andcalculating the target position and orientation of the UAV by taking into account the field of view of the acquisition device. 9. The method according to claim 1, in which a series of images are acquired in order to systematically cover a photographic target from various bearings or elevations, thus defining a series of set of parameters calculated according to the steps of: determining on a map display a photographic target and a width of ground coverage;defining a bearing or elevation resolution determining an angle increment between a plurality of successive bearings or elevations for the UAV; andcalculating each set of parameters by successively changing the bearing or elevation according to a bearing or elevation resolution thus determining a set of successive target positions and orientations of the UAV.
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이 특허에 인용된 특허 (2)
Lissaman, Peter B. S.; Morgan, W. Ray; Cowley, Martyn B.; Sink, Charles J.; Watson, William D., Rapid assembly aircraft for ground surveillance.
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