• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The apparatus comprises a camera (10) with a digital sensor read by a rolling shutter type mechanism delivering video data (Scam) line by line. An exposure control circuit (22) dynamically adjusts the exposure time (texp) according to the illumination level of the captured scene. A gyrometric unit (12) delivers a gyrometric signal (Sgyro) representative of the instantaneous variations of attitude (φ,,, Ψ) of the camera, and a processing circuit (18) which receives the video data (Scam) and the signal Gyrometric (Sgyro) delivers video data processed and corrected artifacts introduced by vibrations specific to the device. An anti-wobble filter (24) dynamically modifies the gain of the gyro signal as a function of the exposure time (texp), so as to reduce the gain of the filter as the exposure time increases, and vice versa.
    公开号:FR3027143A1
    申请号:FR1459720
    申请日:2014-10-10
    公开日:2016-04-15
    发明作者:Pierre Eline；Eng Hong Sron
    申请人:Parrot SA；
    IPC主号:
    专利说明:

    [0001] The invention relates to the processing of digital images captured by an onboard camera in a mobile device, in particular a motorized flying machine such as a drone. The invention advantageously applies to the images collected by the front camera of a rotary wing drone such as a quadrocopter. A typical example of such a drone is the AR.Drone 2.0 from Parrot SA, Paris, France, which is a quadricopter equipped with a series of sensors (accelerometers, 3-axis gyrometers, altimeter), a front camera capturing a image of the scene towards which the drone is directed, and a vertical aiming camera capturing an image of the terrain overflown. The drone is provided with multiple rotors driven by respective engines controllable in a differentiated manner to control the drone attitude and speed. Various aspects of this drone are described in WO 2010/061099 A2, EP 2 364 757 A1 or EP 2,613,214 A1 (Parrot SA). The front video camera is usable for "immersive" control, ie where the user uses the camera image in the same way as if he were himself on board the aircraft. It can also be used to capture sequences of images of a scene towards which the drone is moving, so that the user can use the drone in the same way as a camera or camcorder which, instead of being held by hand, would be carried by the drone.The collected images can be recorded and broadcast, posted on web hosting video sequences, sent to other Internet, shared on social networks, etc. These images are intended to be recorded and communicated, it is desirable that they have the least possible defects, including defects caused by the behavior of the drone, which can generate oscillations, deformations and other artifacts untimely The image captured by the camera may be acceptable in an "immersive steering" configuration. On the other hand, if it is to use the drone in the manner of a mobile video camera to capture sequences that will be recorded and retrieved later, these defects are extremely troublesome, so that it is desirable to reduce to a minimum. The invention is particularly aimed at eliminating the defect known as wobble, which is a blurring effect and deformation of the image. This effect appears in the presence of high frequency and low amplitude vibrations, typically the vibrations of the motors, transmitted to the camera support 5, which result in the deformation of the straight lines with the appearance of waves and formation of waves. the image. This effect, even if it is not very accentuated, is very quickly perceptible to the eye, so that it degrades very quickly the visual quality of the image. This particular artefact is due to the rolling shutter mechanism (and not 10 not global shutter) used by camera sensors such as those embedded on drones, where the lines constituting the image are not acquired at the same time for all the pixels of the image, but one after the other. The vibrations occurring during the capture of an image thus generate within the image deformations that are not the same from one line to the next, hence the appearance of the edulations. The line-by-line correction ("intra-image" correction) of the wobble effect can be performed by using the gyrometer measurements, which deliver a signal representative of the instantaneous rotations of the drone and thus of the camera in the three axes, including rapid variations due to vibration. The application of an inverse transform of the gyrometric measurement makes it possible to compensate to a certain extent the wobble effect, since the attitude of the drone can be acquired precisely for each of the lines, and in synchronism with the sensor. the camera.
    [0002] A technique of this type is described in particular in the application FR 14 56302 of July 2, 2014 for "rotary-wing drone equipped with a video camera delivering stabilized image sequences", in the name of the Applicant. However, as will be explained more precisely in the detailed description below, this method of compensating the wobble by using the gyrometric signal is likely to produce under-conditions over-corrections generating new artifacts, with the consequence that that the corrected image is, paradoxically, more degraded than the raw image obtained before any correction.
    [0003] The starting point of the invention is the observation that this phenomenon is related to the exposure time of the camera, and only occurs with long exposure times, corresponding to dark scenes. Indeed, when the exposure time is close to the vibrating period experienced by the camera (that is to say the vibration that generates the wobble that one seeks to reduce), the wobble is naturally filtered by the long exposure time of the camera. The raw image then presents a blur of shake but little or no ripples. But if a reverse correction is applied from the gyrometric signal - which reflects the effect of the vibration on the camera but does not take into account the filtering effect by the long exposure time - then this reverse correction shows in the image, in addition to the slight motion blur, a ripple that did not exist on the raw image. The basic principle of the invention consists in inserting a filter in the image stabilization chain, between the circuit delivering the gyro-metric signal and the distortion correction circuit, so that the gyrometric signal, reflecting the instantaneous rotation of the camera due to vibration, or filtered with a transfer function depending on the exposure time of the camera for the current image. For each image a filter will be generated with a cutoff frequency that varies inversely with the exposure time, so as to progressively remove from the correction signal (gyrometric signal) the naturally filtered camera movements due to the exposure time. increasing, and thus not introducing false corrections degrading the result.
    [0004] More precisely, the invention proposes a mobile device, in particular a motorized flying machine such as a drone, comprising in a manner known per se a camera comprising an objective, a digital sensor on which an image of a scene is formed. during a given exposure time, and a reading mechanism of the rolling shutter type sensor 30 delivering line-by-line video data, as well as an exposure control circuit, comprising a servo adapted to adjust dynamically the exposure time according to the level of illumination of the captured scene. A gyroelectric unit delivers a gyrometric signal representative of the instantaneous variations of the attitude of the mobile apparatus, and an image processing circuit receiving the video data as input and the gyrometric signal outputting processed video data. and corrected artifacts introduced by vibration specific to the mobile device. In a characteristic manner of the invention, an anti-wobble filter dynamically alters the gain of the gyro signal input to the image processing circuit as a function of the exposure time determined by the exposure control circuit. in order to reduce the gain of the filter when the exposure time increases, and vice versa. According to various advantageous subsidiary characteristics: the filter gain variation law is a monotonic variation law, which can be bounded between a maximum unity gain and a zero minimum gain; the anti-wobble filter is a digital filter capable of generating, for a given image, a low-pass Butterworth filter whose order is pre-defined and whose cutoff frequency varies as a function of the exposure time. determined position for said given image; - The law of variation of the cutoff frequency Fc of the Butterworth filter as a function of the exposure time tee is a law of the type Fc = 1/2. texp; the digital filter is applied to the gyrometric signal twice, in the forward direction and in the return direction; the camera outputs the video data during the duration of an acquisition window, and the anti-wobble filter is applied for a given image during the duration of a processing window starting before the acquisition window of this window; image, and ending after the image acquisition window.
    [0005] An embodiment of the invention will now be described with reference to the accompanying drawings in which the same references designate identical or functionally similar elements from one figure to another. FIGS. 1a-1c illustrate the jelly and wobble artefacts observable on the image of a checkerboard, before application of any corrective filtering.
    [0006] Figures 2a to 2d illustrate the images of a high contrast vertical bar, obtained by applying various distortion correction techniques, with a short exposure time. Figures 3a to 3d illustrate the same respective images as those of Figures 2a to 2d, but with a long exposure time, close to the period of vibration experienced by the camera. Figure 4 illustrates, in block diagram form, the various elements for correcting and filtering wobble-type artifacts according to the invention.
    [0007] Figure 5 illustrates the optimized gain / exposure time characteristic for the characteristic vibration frequency experienced by the camera, as measured experimentally and approximated by a mathematical function to model this optimum characteristic. Figure 6 is a timing chart showing the action of the dynamic filter of the invention, in the case of a captured image with a short exposure time. Figure 7 is the counterpart of Figure 6 for a long exposure time.
    [0008] In Figure 1 there is illustrated the deformations called jelly and wobble observables on the image of a checkerboard shown in Figure la. These artifacts are specific to a rolling shutter type sensor (and not global shutter), where the lines constituting the image are not acquired at the same time for all the pixels of the image, but successively line after line (or group of lines after group of lines), as the sensor sweeps in the direction DB, perpendicular to the lines L. The movements of the drone and the vibrations occurring during the capture of an image thus generate elsewhere in the within the image of deformations that will not be the same from one line to the next. The jelly effect, visible in Figure 1b, appears in the presence of movements of the camera of high amplitude but of relatively low frequency, for example in the presence of large rotations of the drone: when it rotates, between the beginning and the end from the exploration of the sensor by the shutter 3027143 6 rolling shutter, the image will have moved several pixels (in the example of Figure 1b, about a checkerboard tile between the top and bottom of the 'picture). This phenomenon can be overcome by adapting to each line L of the image a suitable offset as the DB sweeps the sensor, this correction line by line to cancel the artefact jelly introduced by the rapid rotation of the drone . Figure 1c illustrates the other type of artifact, called "wobble effect", which is the one concerned by the present invention. Unlike the jelly effect which is a low frequency and high amplitude effect caused by the rotations of the drone to move, the wobble effect is mainly caused by the vibrations of the engine, which introduce oscillations of high frequency (typically of the order of 120 Hz) and low amplitude. The wobble effect is partially corrected by appropriate mechanical damping of the camera support for filtering engine vibration, as described for example in WO 2011/058255 A1 (Parrot SA). This mechanical filtering is, in practice, not sufficient and the residues of the wobble effect must be eliminated, which can be achieved by using measurements delivered by the inertial unit of the drone, representative of the instantaneous rotations of the drone caused by vibrations, and applying corrections line by line. The gyrometers of the inertial unit indeed make it possible to have an indication of the precise attitude of the drone for each of the lines, thus allowing an "intra-image" correction line by line so as to re-align the successive lines, one by to others in order to reproduce an image as close as possible to the captured scene, ie the checkerboard of Figure 1a in this example. The aforementioned French application 14 56302 of July 2, 2014 describes such a technique for correcting the jelly and wobble effects using the signals delivered by the gyrometers of the inertial unit of the drone, a technique which will be described later with reference to FIG. This technique is, however, not disadvantageous in certain circumstances, as will now be explained with reference to Figures 2 and 3.
    [0009] In FIG. 2, a high-contrast scene having a straight line is simulated, with: FIG. 2a, the original scene, that is to say the real representation serving as a reference; 5 - Figure 2b, the image obtained on a rolling shutter type sensor of a camera filming the scene of Figure 2a, and prone to a significant vibration: the initial straight line appears curled because the lines ei are not acquired simultaneously, but scanned successively in the direction DB, according to the characteristic technique of a rolling shutter camera; - Figure 2c, the image of Figure 2b after correction by applying the reverse movement of the vibration, as measured by gyrometers integral with the camera: as can be seen, the ripple has disappeared, at the price only of a slight thickening of the line, which is not annoying for the perception of the image; FIG. 2d, the image of the scene of FIG. 2a that would have been obtained on a global shutter type sensor of a camera filming the scene of FIG. 2a: the lines of the sensor are read in block simultaneously, therefore are not subject to the wobble phenomenon. This type of image 20 constitutes the ideal that we will seek to get closer to. The representations of FIG. 2 were made with a very short exposure time, of the order of 1 ms, corresponding to shooting conditions typical of those that can be encountered outdoors in sunny weather.
    [0010] FIG. 3 illustrates the results that would be obtained with a longer exposure time, for example 8 ms, close to the period of the vibration experienced by the camera (ie 8.33 ms for a vibration at 120 Hz). It can be seen in Figure 3b that the wobble has been naturally filtered by the camera: the ripple has disappeared and the artifact only manifests itself in the form of a progressive blur, which is not too visually disturbing. This result is moreover quite comparable, as illustrated in Figure 3d, to what one would have obtained with a global shutter type sensor which would also present a motion blur at the level of the contrast zone. On the other hand, as illustrated in FIG. 3c, the image on which the inverse movement undergone by the camera and measured by the gyrometer has been applied results in a poor quality result, very far from the ideal constituted by the image of Figure 3d that we would have with a global shutter sensor. This example demonstrates the limits of the anti-wobble correction by applying an inverse gyrometric signal: the gyrometers measure, certainly, all the movements experienced by the camera during the scanning of the image of the sensor but, according to the frequency of these movements and exposure time, these movements are likely to generate more or less visible deformations, which have the effect of over-correcting certain movements and generating new artifacts. By applying a correction, one thus paradoxically obtains an image of poorer quality (FIG. 3c) than if no correction had been applied (FIG. 3b). This is the problem that the present invention aims to solve. FIG. 4 illustrates, in block diagram form, the various elements of an image processing circuit for correcting the wobble effect on the image signal Scam delivered by a camera 10 comprising an image sensor. rolling shutter type. This camera is subject to angular displacements, of great amplitude and low frequency (displacement of the drone) as well as of low amplitude and high frequency (vibration of the engines). These movements 20 experienced by the camera are measured by an inertial unit 12 whose measurements are applied to a circuit 14 for estimating the attitude of the drone delivering a Sgyro gyrometric signal representative of the instantaneous rotations of the drone and therefore of the camera, the inertial unit 12 and the camera 10 being mechanically secured. These rotations are given by the pitch angle (I), the roll angle θ and the yaw angle y describing the inclination of the drone in the three dimensions relative to a fixed terrestrial reference ( Euler angle). The gyrometric signal Sgyro is applied to a circuit 18 for stabilizing and correcting the artifacts of the image signal Scam, in order to obtain at output a corrected and stabilized image signal which can then be transmitted to the user for visualization on a satellite. screen, save to a digital memory, etc. The camera 10 and the inertial unit 12 are driven by a common clock circuit 16, the respective operating frequencies of the inertial unit and the camera being sub-multiples of the frequency CLK of this In other words, the camera 10 and the inertial unit 12 are configured so that Fgyro = K.Fcam, Fgyro being the acquisition frequency of the gyrometers (typically Fgyro = 990 Hz), Fcam being the frequency acquisition of the images by the video camera (Typically, Fcam = 30 Hz), and K being a positive integer (typically, K = 33). The fact that K is an integer and that the base clock is the same for the gyrometers and the camera ensures that there will always be K samples of the Sgyro gyro signal per Scam image, without any drift, the angle measurements falling always at the same moment.
    [0011] However, if this mechanism ensures that the Sgyro signal delivered by the gyro sensors and the Scam signal delivered by the camera are synchronous, it gives no guarantee as to the phase concordance of these signals. To ensure perfect synchronization, a hardware component 20 measures the time interval A between the Sgyro and video Scam gyrometric signals with high accuracy. The common clock 16 and the hardware circuit 20 for measuring the phase shift thus make it possible to connect the gyrometric and video signals in a very accurate time, to a close clock cycle. Note that a single measurement is sufficient since the clocks have been set so that they do not drift. This configuration is that described in the above-mentioned application FR 14 56302 but, as seen with reference to FIGS. 2 and 3, in the case of long exposure times it does not make it possible to obtain a satisfactory correction of the wobble, on the contrary, it introduces new artifacts by over-correction effect. For this, the present invention proposes to dynamically modulate the effect of the gyrometric correction, as a function of the exposure time of the image. The exposure time texp is determined, image by image, by an exposure control circuit 22, including a servo-control for dynamically adjusting the exposure time according to the level of illumination of the scene captured by According to this level of illumination, determined by analysis of the Scam signal, the circuit 22 drives the camera so as to vary the exposure time to maintain the level of illumination in the best conditions. condition of rendering the image by the sensor. Characteristically, the invention provides for interposing between the inertial unit 12 and the digital correction circuit of the image 18 a dynamically controlled filter 24 as a function of the exposure time t e determined by the circuit 22. This filtering is an adaptive filtering with, for each image, generating a digital filter whose cutoff frequency will vary in the opposite direction of the exposure time, so as to further reduce the gyrometric signal - and therefore the correction that it It introduces into the image that the exposure time will be high, so as not to introduce false correction degrading the result. With reference to FIG. 5, the manner in which the transfer function of this filter is defined will now be explained. In the first place, the optimal attenuation to be applied to the Sgyro data from the gyrometers as a function of the frequency of the helices is experimentally determined for different exposures (in an implementation example, in a fixed point the helices rotate to 120 Hz, and it is this frequency value that will be used to adjust the characteristics of the dynamic filter).
    [0012] To do this, the drone is flown in front of a test pattern, the result produced for different attenuation values of the Sgyro signal is examined, and the amplitude of the undulations of the image is measured: when this amplitude is minimal, it is considered that the optimum gain value A1 has been found. The different values A1, A2 ... A7 recorded for increasing exposure times of 3 ms, 4 ms ... 10 ms give the optimum gain curve shown in Figure 5. As can be seen, for Exposure time less than 3 ms the gain is equal to unity, i.e. the entire Sgyro signal reflecting the vibration of the helices is applied to the artifact correction circuit 18 without filtering. On the other hand, for exposure times equal to or greater than 8 ms, the Sgyro signal is totally filtered, that is to say that the gyrometric signal is not taken into account at all to correct the artifacts. Between the two, for an average exposure time of 5 ms, the best gain is about 0.5, which means that the magnitude of the Sgyro correction signal must be halved.
    [0013] The next step is to model the characteristic measured experimentally, that is to say to determine the generation law of the digital filter that will be applied to each image. One can advantageously choose a Butterworth type filter for the quality of its gain response which is as constant as possible in the bandwidth. To overcome the phase shift problems, the filter is applied twice to the Sgyro gyrometric data, first in the forward direction and then in the reverse direction. More precisely: the gyrometric signal produces a series of samples e 0, e 1. the filter is applied a first time to this sample, giving filtered values Fo, F1-Fn; the order of these values is reversed, giving a sequence Fn ... F1, Fo; the filter is applied a second time, producing new filtered values F'4. ". F'1, Po; and the order of these samples is inverted to give the values Po, F'1 ... Pn which will finally be used by the artefact correction circuit (filtered Sgyro signal). This dual filtering requires samples of the Sgyro raw gyrometric signal before and after image capture. The anti-wobble treatment will therefore be delayed by a few milliseconds, the time to accumulate in a buffer enough samples of the gyrometric signal. The synthesis of a low-pass Butterworth filter involves two input parameters: its cutoff frequency, beyond which the signals must be attenuated, and its order, which determines the width of the transition band. between the bandwidth and the cut band, that is to say the more or less abrupt nature of this transition.
    [0014] By choosing an order 2 and fixing for the cutoff frequency a law of the type: Fc = 1 / 2.tee, F, being the cutoff frequency of the Butterworth filter and 35 tee being the current value of the exposure time The continuous curve of the modeled gain illustrated in FIG. 5 is obtained, which compares the characteristic measured experimentally quite suitably. Figures 6 and 7 are timing diagrams showing the action of the dynamic filter of the invention, in the case of an image captured respectively with a short exposure time and a long exposure time. In these figures, the area A corresponds to the acquisition window of the image, and the "Sgyro (gross)" curve corresponds to the gyrometric signal before filtering is applied.
    [0015] In order to effect the correction according to the invention, it is necessary to collect a history of the samples of the gyrometric signal over a larger window (earlier samples P and later samples P ') than the window A corresponding to the only data of the image. Figure 6 illustrates a case where the exposure time is short, with the filter partially applied so as to reduce the effect of the vibrations. By comparing the two curves "Sgyro (gross)" and "Sgyro (filtered)", it can be seen that the low frequency ripples have been preserved and the high frequencies are partially attenuated, all without phase shift. FIG. 7 is a counterpart of FIG. 6, in the case of a very long exposure time: in this case, the high frequency of the gyrometric signal is completely suppressed by the filter. In contrast, low frequency variations are preserved. These slow variations, representative of a fel 'effect, can be corrected by a conventional technique of line-to-line registration of the successive lines of the image.
    权利要求:
    Claims (8)
    [0001]
    REVENDICATIONS1. A mobile device, in particular a motorized flying machine such as a drone, comprising: a camera (10) comprising an objective, a digital sensor on which an image of a scene is formed during a given exposure time (texp) , and a rolling shutter type sensor reading mechanism delivering line-by-line output of video data (Scam); an exposure control circuit (22) comprising a servo adapted to dynamically adjust the exposure time (texp) as a function of the level of illumination of the captured scene; a gyrometric control unit (12) capable of delivering a gyrometric signal (Sgyro) representative of the instantaneous variations of the attitude (p, 6, p) of the mobile device; an image processing circuit (18); ), receiving as input the video data (Scam) and the gyrometric signal (Sgyro), and outputting video data processed and corrected artifacts introduced by vibrations specific to the mobile device, characterized in that it further comprises: an anti-wobble filter (24), able to dynamically modify the gain of the gyrometric signal applied at the input of the image processing circuit as a function of the exposure time (texp) determined by the control circuit exposure, so as to reduce the gain of the filter when the exposure time increases, and vice versa.
    [0002]
    2. The mobile apparatus of claim 1, wherein the filter gain variation law is a law of monotonic variation.
    [0003]
    The mobile apparatus of claim 2, wherein the filter gain variation law is a variation law bounded between a maximum unity gain and a zero minimum gain.
    [0004]
    4. The mobile apparatus of claim 2, wherein the anti-wobble filter (24) is a digital filter adapted to generate, for a given image, a low-pass Butterworth filter whose order is predefined and whose Frequency of cut (Fa) varies according to the exposure time (texp) determined for said given image.
    [0005]
    5. The mobile apparatus of claim 4, wherein the law of variation of the Butterworth filter cut-off frequency Fc as a function of the exposure time tee is a Fc = 1 / 2.texp type law.
    [0006]
    The mobile apparatus of claim 4, wherein the digital filter is applied to the gyro signal twice, in the forward direction and in the reverse direction.
    [0007]
    The mobile apparatus of claim 1, wherein the camera is capable of outputting the video data during the duration of an acquisition window (A), and wherein means are provided for applying the anti-wobble filter for a given image during the duration of a processing window (P, A, P ') beginning before the acquisition window of this image.
    [0008]
    8. The mobile apparatus of claim 7, wherein said means is adapted to apply the anti-wobble filter for the duration of said treatment window (P, A, P ') ending after the window. image acquisition.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3007429B1|2016-12-28|Mobile apparatus, in particular a rotary-wing drone, provided with a video camera supplying image sequences with dynamic correction of the wobble effect
    EP3171589B1|2018-06-06|Drone equipped with a video camera sending sequences of images corrected for the wobble effect
    EP3048789B1|2016-12-28|Drone provided with a video camera and means to compensate for the artefacts produced at the greatest roll angles
    EP3142354B1|2018-03-14|Drone with forward-looking camera with segmentation of the image of the sky in order to control the autoexposure
    EP2933775B1|2016-12-28|Rotary-wing drone provided with a video camera supplying stabilised image sequences
    EP3142353B1|2019-12-18|Drone with forward-looking camera in which the control parameters, especially autoexposure, are made independent of the attitude
    EP3113103A1|2017-01-04|High-resolution camera unit for drone, with correction of wobble distortion
    US9762799B2|2017-09-12|Received video stabilization
    EP2753971B1|2015-07-01|Stabilization of a line of sight of an imaging system embedded onboard a satellite
    EP3142356A1|2017-03-15|Method for determining an exposure time of a camera mounted on a drone, and associated drone
    EP1298592B1|2014-04-16|Stabilizing images of a scene, gray level offset correction, moving object detection and adjustment of two image pickup devices based on image stabilization
    EP0033172B1|1985-04-24|Circuit for correcting the phase differences between the deflection control signals and the synchronisation signals in a television receiver
    EP3114831B1|2021-06-09|Optimised video denoising for heterogeneous multisensor system
    EP3054422A1|2016-08-10|Method for determining an axis of rotation of a tomography object and method for characterisation by tomography
    EP0629082B1|1999-02-03|Spatial correction method of digital images
    FR3052678A1|2017-12-22|DRONE PROVIDED WITH A FRONTAL VIDEO CAMERA COMPRESSING THE INSTANTANEOUS ROTATIONS OF THE DRONE AND CORRECTION OF THE ARTIFACTS
    FR2968499A1|2012-06-08|METHOD OF USING IMAGE SENSOR
    FR2863750A1|2005-06-17|Images stabilizing method for e.g. smear camera, involves subjecting each line or column to inverse rotation or translation for stabilizing with respect to adjacent line or column, according to rotational and translatory movement of block
    FR2999735A1|2014-06-20|IMAGE ACQUISITION METHOD AND DEVICE
    FR3020168A1|2015-10-23|ROTATING WING DRONE WITH VIDEO CAMERA DELIVERING STABILIZED IMAGE SEQUENCES
    EP2747420A2|2014-06-25|Method for motion compensation in a plurality of image sequences
    同族专利:
    公开号 | 公开日
    JP2016082589A|2016-05-16|
    US9826202B2|2017-11-21|
    CN105516583A|2016-04-20|
    EP3007429A1|2016-04-13|
    FR3027143B1|2016-11-11|
    US20160105648A1|2016-04-14|
    EP3007429B1|2016-12-28|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US20040056963A1|2002-09-24|2004-03-25|Yoshikazu Ishikawa|Vibration correction for image sensing apparatus|
    US20080030587A1|2006-08-07|2008-02-07|Rene Helbing|Still image stabilization suitable for compact camera environments|
    US20110129166A1|2009-11-30|2011-06-02|Canon Kabushiki Kaisha|Image processing apparatus and image processing method|
    US20120242847A1|2011-03-22|2012-09-27|Canon Kabushiki Kaisha|Image sensing apparatus for correcting image distortion caused by hand shake, and control method thereof|
    US20130044230A1|2011-08-15|2013-02-21|Apple Inc.|Rolling shutter reduction based on motion sensors|
    CA792305A|1964-12-03|1968-08-13|N.V. Philips Gloeilampenfabrieken|Transmitting arrangement for use in tone frequency pushbutton selection systems|
    JP3829843B2|2003-12-08|2006-10-04|ソニー株式会社|Image processing device|
    JP4530961B2|2005-06-30|2010-08-25|オリンパスイメージング株式会社|Electronic image stabilization device|
    CN101518054B|2006-09-25|2012-11-21|高通股份有限公司|A hand jitter reduction system for cameras|
    FR2938774A1|2008-11-27|2010-05-28|Parrot|DEVICE FOR CONTROLLING A DRONE|
    FR2952787B1|2009-11-13|2012-07-27|Parrot|ELECTRONIC NAVIGATON CARD HOLDER FOR ROTARY SAIL DRONE|
    FR2957266B1|2010-03-11|2012-04-20|Parrot|METHOD AND APPARATUS FOR REMOTE CONTROL OF A DRONE, IN PARTICULAR A ROTATING SAIL DRONE.|
    FR2985581B1|2012-01-05|2014-11-28|Parrot|METHOD FOR CONTROLLING A ROTARY SAILING DRONE FOR OPERATING A SHOOTING VIEW BY AN ON-BOARD CAMERA WITH MINIMIZATION OF DISTURBING MOVEMENTS|
    JP6087671B2|2013-03-12|2017-03-01|キヤノン株式会社|Imaging apparatus and control method thereof|
    EP2974269B1|2013-03-15|2018-07-25|Freefly Systems Inc.|Method and system for enabling pointing control of an actively stabilized camera|
    JP6242145B2|2013-10-10|2017-12-06|キヤノン株式会社|Image shake correction apparatus, control method thereof, and imaging apparatus|CN106797438B|2014-10-17|2020-03-06|索尼公司|Control device, control method and aircraft device|
    US9934559B2|2016-02-19|2018-04-03|Fotonation Limited|Method for correcting an acquired image|
    CN108605098B|2016-05-20|2020-12-11|深圳市大疆创新科技有限公司|System and method for rolling shutter correction|
    FR3052556B1|2016-06-13|2018-07-06|Parrot Drones|IMAGING ASSEMBLY FOR DRONE AND SYSTEM COMPRISING SUCH AN ASSEMBLY MOUNTED ON A FLYING DRONE|
    BR112019005759A2|2016-09-23|2019-06-11|Qualcomm Inc|image processing on an unmanned autonomous vehicle|
    WO2018053786A1|2016-09-23|2018-03-29|Qualcomm Incorporated|Adaptive motion filtering in an unmanned autonomous vehicle|
    US20180186471A1|2017-01-03|2018-07-05|Qualcomm Incorporated|360 Degree Camera Mount for Drones and Robots|
    CN108120452B|2017-12-21|2021-12-24|吉林大学|Filtering method for dynamic data of MEMS gyroscope|
    EP3550506B1|2018-04-05|2021-05-12|Everdrone AB|A method for improving the interpretation of the surroundings of a uav, and a uav system|
    WO2020220292A1|2019-04-30|2020-11-05|深圳市大疆创新科技有限公司|Electronic image stabilization method, image acquisition device and movable platform|
    CN110636223B|2019-10-16|2021-03-30|Oppo广东移动通信有限公司|Anti-shake processing method and apparatus, electronic device, and computer-readable storage medium|
    WO2021138768A1|2020-01-06|2021-07-15|深圳市大疆创新科技有限公司|Method and device for image processing, movable platform, imaging apparatus and storage medium|
    法律状态:
    2015-10-22| PLFP| Fee payment|Year of fee payment: 2 |
    2016-04-15| PLSC| Publication of the preliminary search report|Effective date: 20160415 |
    2016-10-20| PLFP| Fee payment|Year of fee payment: 3 |
    2016-11-11| TP| Transmission of property|Owner name: PARROT DRONES, FR Effective date: 20161010 |
    2017-10-19| PLFP| Fee payment|Year of fee payment: 4 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1459720A|FR3027143B1|2014-10-10|2014-10-10|MOBILE APPARATUS, IN PARTICULAR ROTATING SAIL DRONE, PROVIDED WITH A VIDEO CAMERA DELIVERING IMAGE SEQUENCES DYNAMICALLY CORRECTED BY THE "WOBBLE" EFFECT|FR1459720A| FR3027143B1|2014-10-10|2014-10-10|MOBILE APPARATUS, IN PARTICULAR ROTATING SAIL DRONE, PROVIDED WITH A VIDEO CAMERA DELIVERING IMAGE SEQUENCES DYNAMICALLY CORRECTED BY THE "WOBBLE" EFFECT|
    US14/855,287| US9826202B2|2014-10-10|2015-09-15|Mobile appratus, in particular a rotary-wing drone, provided with a video camera delivering sequences of images dynamically corrected for the wobble effect|
    CN201510783482.7A| CN105516583A|2014-10-10|2015-09-25|Mobile appratus, in particular rotary-wing drone, provided with video camera delivering sequences of images dynamically corrected for the wobble effect|
    EP15187543.2A| EP3007429B1|2014-10-10|2015-09-30|Mobile apparatus, in particular a rotary-wing drone, provided with a video camera supplying image sequences with dynamic correction of the wobble effect|
    JP2015200693A| JP2016082589A|2014-10-10|2015-10-09|Mobile apparatus, in particular, rotary-wing drone, provided with video camera supplying image sequences with dynamic correction of wobble effect|
    [返回顶部]