`
`PATENT
`Attorney Docket No. 45236-734.301
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`IN THE UNITED STATES PATENT AND TRADEMARK OFFICE
`
`In re Application:
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`Inventor: Bo Zang
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`Application No.: 14/471,954
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`Filing Date: August 28, 2014
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`Title: SYSTEMS AND METHODS FOR TARGET
`TRACKING
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`Confirmation No.: 7890
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`Examiner: Peter D. Nolan
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`Group Art Unit: 3661
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`Customer No.: 021971
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`Mail Stop Amendment
`Commissioner of Patents
`P.O. Box 1450
`Alexandria, VA 22313-1450
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`SUPPLEMENTAL AMENDMENT AND
`RESPONSE TO NON-FINAL OFFICE ACTION
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`Sir:
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`This paper supplements the Amendment and Response to Non-Final Office Action filed
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`on April 6, 2015. Applicants respectfully request reconsideration of the above-referenced
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`application in view of the following amendments and remarks.
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`Amendments to Claims begin on page 2 of this paper.
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`Remarks begin on page 9 of this paper.
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`7321479_1.docx
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`Yuneec Exhibit 1006 Page 1
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`Serial No. 14/471,954
`Non-Final Office Action Mailed On January 5, 2015
`Supplemental Amendment And Response To Non-Final Office Action Filed May 7, 2015
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`Amendments to the Claims:
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`1.
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`(Currently Amended) A system for controlling an unmanned aerial vehicle (UA V),
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`comprising:
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`one or more receivers, individually or collectively, configured to receive from a remote user
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`(1) one or more navigation commands to move the UAV along a flight path, and (2) target
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`information of a target to be tracked by an imaging device on the UA V; and
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`one or more processors, individually or collectively, configured to track the target according
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`to the target information by automatically adjusting at least one of the UAV or the imaging device
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`while the UA V moves along the flight path according to the one or more navigation commands from
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`the remote user, wherein the one or more processors, individually or collectively, make a
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`determination to adjust 1) the UAV, 2) the imaging device, or 3) both the UAV and the imaging
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`device, wherein said determination is dependent upon a) number of rotational axis of the imaging -
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`device and orientation of said rotational axis relative to the UAV; b) a navigation path of the UAV;
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`or c) a maximum angular speed allowable for the UAV or the imaging device 'tvherein the adjustment
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`involves adjusting an angular velocity of the UA.V relative to a yaw axis or pitch mds of the UAV,
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`and wherein an absolute value of the angular velocity being adjusted depends on a deviation in
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`distance benveen an eKpected and actual position of the target in an image captured by the imaging
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`de\4ee.
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`2.
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`(Original) The system of claim 1, wherein the target information comprises initial
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`target information comprising an initial position or an initial size of the target within an image
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`captured by the imaging device.
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`3.
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`(Original) The system of claim 1, wherein the target information comprises target
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`type information comprising color, texture, or pattern information.
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`4.
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`(Original) The system of claim 3, wherein tracking the target according to the target
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`information further comprises identifying, based on the target type information, the target to track
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`from within one or more images captured by the imaging device using an image recognition
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`algorithm.
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`5.
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`(Original) The system of claim 1, wherein the target information comprises expected
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`target information comprising an expected position or an expected size of the target within an image
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`captured by the imaging device.
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`6.
`
`7.
`
`(Canceled)
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`(Original) The system of claim 1, wherein the imaging device is coupled to the UA V
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`via a carrier configured to permit the imaging device to rotate around at least two axes relative to the
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`UAV.
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`8.
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`(Original) The system of claim 7, wherein the target information comprises expected
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`target information and tracking the target according to the target information comprises:
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`determining current target information of the target based on one or more images captured by
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`the imaging device;
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`detecting a deviation of the current target information from the expected target information;
`
`and
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`calculating an adjustment to the UAV, the carrier, or the imaging device so as to substantially
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`correct the deviation.
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`9.
`
`(Previously Presented) The system of claim 8, wherein the deviation is related to a
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`change in position of the target and the calculated adjustment is related to an angular velocity for the
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`imaging device relative to a yaw axis or a pitch axis of the imaging device.
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`10.
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`(Original) The system of claim 9, wherein the calculated adjustment is used to
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`generate control signals for the carrier so as to cause the imaging device to move relative to the
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`UAV.
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`11.
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`(Canceled)
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`Supplemental Amendment And Response To Non-Final Office Action Filed May 7, 2015
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`12.
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`(Previously Presented) The system of claim 8, wherein the one or more processors are
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`configured to provide a warning signal ifthe adjustment falls outside a predetermined range
`
`corresponding to a predetermined range of control lever amount of a control system comprising a
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`navigation control system for the UA V or a control system for the carrier.
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`13.
`
`(Currently Amended) A method for controlling an unmanned aerial vehicle
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`(UA V), comprising:
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`receiving, from a remote user, user-specified target information of a target to be tracked
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`by an imaging device on the UA V, the user-specified target information including a
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`predetermined position or predetermined size of the target within an image captured by the
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`imaging device, the imaging device coupled to the UA V via a carrier configured to permit the
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`imaging device to move relative to the UAV;
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`detecting, by one or more processors onboard the UAV, a deviation from the predetermined
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`position or the predetermined size of the target based on one or more images captured by the imaging
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`device; and
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`automatically adjusting the UAV, the carrier, or the imaging device so as to substantially
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`correct the detected deviation from the predetermined position or the predetermined size of the target,
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`wherein the one or more processors, individually or collectively, make a determination to adjust 1)
`
`the UA V, 2) the imaging device, or 3) both the UA V and the imaging device, wherein said
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`determination is dependent upon a) a navigation path of the UAV; orb) a maximum linear speed
`
`allowable for the UAVwherein the adjustment involves adjusting a linear velocity of the UAV that is
`
`dependent upon the detected deviation from the predetermined size of the target ·.vithin the image.
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`14.
`
`(Canceled)
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`15.
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`(Original) The method of claim 13, wherein the predetermined position of the target
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`comprises an initial position or an expected position of the target and the predetermined size of the
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`target comprises an initial size or an expected size of the target.
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`16.
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`(Original) The method of claim 13, wherein detecting the deviation from the
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`predetermined position or the predetermined size of the target comprises comparing a position or size
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`of the target within the one or more images captured by the imaging device with the predetermined
`
`position or predetermined size, respectively.
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`17.
`
`(Currently Amended) The method of claim 13, wherein adjusting the UAV, the
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`carrier, or the imaging device comprises calculating an adjustment to the UAV, the carrier, or the
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`imaging device so as to substantially correct the deviation the adjustment involves adjusting a linear
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`velocity of the UAV that is dependent upon the detected deviation from the predetermined size of the
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`target within the image.
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`18.
`
`(Canceled)
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`19.
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`(Original) The method of claim 17, wherein the deviation is related to a change in size of
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`the target and the adjustment is related to a linear velocity for the UA V or one or more parameters of the
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`imaging device and wherein the one or more operational parameters of the imaging device comprise focal
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`length, zoom level, imaging mode, image resolution, focus, depth of field, exposure, lens speed, or field
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`of view.
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`20.
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`(Original) The method of claim 13, further comprising providing a warning signal if
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`the adjustment falls outside a predetermined range corresponding to a predetermined range of control
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`lever amount of a control system comprising a navigation control system for the UA Vora control
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`system for the carrier.
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`21.
`
`(Original) The method of claim 13, further comprising transmitting, in substantially
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`real-time, images captured by the imaging device to a remote user device accessible to the remote
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`user, the remote user device comprises a display for displaying the images captured by the imaging
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`device and an input device for providing the target information comprising a touchscreen, joystick,
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`keyboard, mouse, stylus, or a wearable device.
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`Supplemental Amendment And Response To Non-Final Office Action Filed May 7, 2015
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`22.
`
`(Currently Amended) An apparatus for controlling an unmanned aerial vehicle
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`(UA V), comprising:
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`a display configured to display one or more images captured by an imaging device coupled
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`to the UAV;
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`an input device configured to receive a user selection of a target from within at least one of
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`the one or more images being displayed on the display;
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`one or more processors, individually or collectively, configured to generate target
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`information of the target based at least in part on the user selection of the target; and
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`a transmitter configured to provide the target information to the UA V so as to allow the UA V
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`to autonomously track the target according to the target information, wherein the one or more
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`processors, individually or collectively, make a determination to adjust 1) the UA V, 2) the imaging
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`device, or 3) both the UA V and the imaging device, wherein said determination is dependent upon a)
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`number of rotational axis of the imaging device and orientation of said rotational axis relative to the
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`UAV; b) a navigation path of the UAV; or c) a maximum angular speed allowable for the UAV or
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`the imaging device and by adjusting an angular velocity of the UAV according to a deviation in
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`distance bet\veen an expected and actual position of the target in the one or more images being
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`displayed on the display.
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`23.
`
`(Original) The apparatus of claim 22, wherein the target information comprises initial
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`target information, target type information, and/or expected target information.
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`24.
`
`(Canceled)
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`25.
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`(Original) The apparatus of claim 22, wherein the user selection of the target is
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`achieved by a user selecting an area of the at least one of the one or more images being displayed on
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`the display, the selected area corresponding to the target.
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`26.
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`(Original) The apparatus of claim 22, wherein the one or more processors,
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`individually or collectively, are further configured to display, on the display, the selected target with
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`a selection indicator in response to the user selection of the target, the selection indicator indicating
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`that the target has been selected by the user.
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`27.
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`(Previously Presented) A system for controlling an unmanned aerial vehicle
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`(UA V), comprising:
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`a receiver configured to receive, in substantially real-time, one or more images captured by
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`an imaging device coupled to the UA V;
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`an input device configured to receive user-specified target information of a target including a
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`predetermined position or a predetermined size of a target within an image from the one or more
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`images;
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`a transmitter for providing the user-specified target information to the UA V, and the user's
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`input on allocation of control over a tracking process between the user and an onboard processing
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`system ofthe UAV; and
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`a display configured to display the one or more images and a tracking indicator associated
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`with the target within the one or more images, the tracking indicator indicating that the target is being
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`tracked by the UAV in substantially real-time according to the user-specified target information.
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`28.
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`(Original) The system of claim 27, wherein the imaging device is coupled to the
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`UAV via a carrier configured to permit the imaging device to rotate relative to the UAV along at
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`least one axis and wherein the input device is further configured to receive one or more commands
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`adapted to control a speed, position, orientation or attitude of the UAV and/or the carrier.
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`29.
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`(Original) The system of claim 28, wherein the target is tracked by the imaging
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`device according to the target information via automatic adjustment to at least one of the UAV, the
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`carrier, or the imaging device.
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`30.
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`(Original) The system of claim 27, wherein the predetermined position comprises an
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`initial or expected position of the target and the predetermined size comprises an initial or
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`expected size of the target.
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`31.
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`(Currently Amended) The system of claim 1, wherein the angular velocity is directly
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`proportional to the deviation in distance bet\veen the expected and actual positionUA V comprises a
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`plurality of rotors configured to generate lift for the UAV.
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`32.
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`(Currently Amended) The system of claim I ,wherein the one or more processors,
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`individually or collectively, makes a determination as to adjust 1) the UAV, 2) the imaging device, or
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`3) both the UAV and the imaging device, wherein said determination is dependent upon a) a number
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`and orientation of rotational axis of the imaging device relative to the UAV; b) a navigation path of
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`the UAV; or c) a maximum angular speed allowable for the UA V or the imaging device.
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`33.
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`(Currently Amended) The method of claim 13, ·.vherein the one or more processors,
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`individually or collectively, makes a determination as to adjust 1) the UAV, 2) the imaging device, or
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`3) both the UAV and the imaging device, wherein said determination is dependent upon aj-a
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`navigation path of the UAV; orb) a maximum linear speed allowable for the UAV; or c) maximum
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`zoom level or focal length allmvable for the imaging device.
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`34.
`
`(Currently Amended) The method of claim 13, wherein the linear velocity is linearly
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`proportional to the detected deviation from the predetermined size of the target within the
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`tm-ageUA V comprises a plurality of rotors configured to generate lift for the UAV.
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`35.
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`(Previously Presented) The system of claim of 27, wherein the system is configured
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`to dynamically adjust the allocation of the control over the tracking process between the user and the
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`UA V based upon a surrounding of the UA V, speed, altitude, computer resource available on board or
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`off board the UAV.
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`Supplemental Amendment And Response To Non-Final Office Action Filed May 7, 2015
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`REMARKS:
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`Upon entry of this amendments, claims 1-5, 7-10, 12, 13, 15-17, 19-23, and 25-35 will be
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`pending and at issue in the present application. Claims 6, 11, 14, 18, and 24 are canceled
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`without prejudice. Claims 1, 13, 17, 22, and 31-34 are amended. Support for the claim
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`amendments can be found in the application as originally filed. See, e.g., paragraphs 0170, 0180,
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`0230, and 0253 and claim 9 as originally filed. No new matter has been added. Reconsideration
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`is respectfully requested in light of the following remarks.
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`Examiner Interview
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`Applicants thank Examiner Nolan for the helpful and courteous in-person interview
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`conducted on April 20, 2015. Examiner Peter D. Nolan, Daijun Zhou, Karen Wong, and Elaine
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`Kim, representatives of the Applicants were in attendance. During the interview, the cited art
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`and proposed amendments to the claims were discussed. Examiner agreed that proposed
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`amendments would advance prosecution.
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`Claim Objections
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`Claims 12, 23, were 27 were objected to due to alleged informalities. Claims 12, 23, and
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`27 were previously amended in the Response to Non-Final Office Action filed on April 6, 2015
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`as suggested by the Examiner. Withdrawal of this objection is respectfully requested.
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`Claims Rejections Under 35 U.S.C. §102
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`Claims 1-6, 13, 14, 16-18, and 20-25 were rejected under 35 U.S.C. 102(a)(l) as
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`allegedly being anticipated by Bevirt (US 2012/0287274 Al).
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`Independent claim 1 is directed to a system for controlling an unmanned aerial vehicle.
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`Claim 1 as amended recites in part that "the one or more processors, individually or collectively,
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`make a determination to adjust 1) the UAV, 2) the imaging device, or 3) both the UA V and the
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`imaging device, wherein said determination is dependent upon a) number of rotational axis of the
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`imaging device and orientation of said rotational axis relative to the UAV; b) a navigation path of the
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`UAV; or c) a maximum angular speed allowable for the UAV or the imaging device." Independent
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`claim 22 recites similar elements. Independent claim 13 recites in part "automatically adjusting
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`the UA V, the carrier, or the imaging device so as to substantially correct the detected deviation from
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`the predetermined position or the predetermined size of the target, wherein the one or more
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`processors, individually or collectively, make a determination to adjust 1) the UAV, 2) the imaging
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`device, or 3) both the UA V and the imaging device, wherein said determination is dependent upon a)
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`a navigation path of the UAV; orb) a maximum linear speed allowable for the UAV." These
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`elements and/or others are missing from Bevirt.
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`Bevirt discloses a system for tracking and video surveillance using an aerial videographic
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`platform (Bevirt, Abstract). The aerial platform may "record from a prescribed position, or on a
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`given trajectory pattern either relative to the OoI location, or relative to a fixed reference
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`location" and "may track the user using a GPS offset" (Bevirt, paragraphs [0015], [0018]).
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`Nothing in the cited disclosure of Bevirt teaches or that the one or more processors, individually or
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`collectively, make a determination to adjust 1) the UAV, 2) the imaging device, or 3) both the UAV
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`and the imaging device, wherein said determination is dependent upon a) number of rotational axis of
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`the imaging device and orientation of said rotational axis relative to the UA V; b) a navigation path of
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`the UAV; or c) a maximum angular speed allowable for the UAV or the imaging device, as recited
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`in claim 1 and 22. Furthermore, nothing in the cited disclosure of Bevirt teaches or suggests a
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`method to automatically adjust the UAV comprising automatically adjusting the UAV, the carrier,
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`or the imaging device so as to substantially correct the detected deviation from the predetermined
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`position or the predetermined size of the target, wherein the one or more processors, individually or
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`collectively, make a determination to adjust 1) the UAV, 2) the imaging device, or 3) both the UAV
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`and the imaging device, wherein said determination is dependent upon a) a navigation path of the
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`UAV; orb) a maximum linear speed allowable for the UAV, as recited in claim 13.
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`Accordingly, one or more elements of independent claims 1, 13, and 22 are missing from
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`Bevirt. Therefore, claims 1, 13, 22, and claims dependent therefrom, are novel over Bevirt.
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`Withdrawal of this rejection is respectfully requested.
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`Claims Rejections Under 35 U.S.C. §103
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`Claims 7-12, 15 and 19 were rejected under 35 U.S.C. 103 as allegedly being
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`unpatentable over Bevirt in view of Lee et al. (US 2012/0307042 Al).
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`Claims 7-12 are directly or indirectly dependent upon claim 1, which recites that the one
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`or more processors, individually or collectively, make a determination to adjust I) the UAV, 2) the
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`imaging device, or 3) both the UAV and the imaging device, wherein said determination is dependent
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`upon a) number of rotational axis of the imaging device and orientation of said rotational axis
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`relative to the UAV; b) a navigation path of the UAV; or c) a maximum angular speed allowable for
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`the UA V or the .imaging device. Claims 15 and 19 are directly or indirectly dependent upon claim
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`13, which recites automatically adjusting the UAV, the carrier, or the imaging device so as to
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`substantially correct the detected deviation from the predetermined position or the predetermined size
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`of the target, wherein the one or more processors, individually or collectively, make a determination
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`to adjust 1) the UAV, 2) the imaging device, or 3) both the UAV and the imaging device, wherein
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`said determination is dependent upon a) a navigation path of the UAV; orb) a maximum linear speed
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`allowable for the UAV. As previously discussed, these elements and/or others are missing from
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`Bevirt.
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`Lee fails to cure the deficiencies of Bevirt. Lee discloses adjustments that are related to
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`"a flight height and a flight orientation" of a UAV (Lee, paragraph [0009]). Nothing in the cited
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`disclosure of Lee even hints that the one or more processors, individually or collectively, make a
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`determination to adjust 1) the UAV, 2) the imaging device, or 3) both the UAV and the imaging
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`device, wherein said determination is dependent upon a) number of rotational axis of the imaging
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`device and orientation of said rotational axis relative to the UA V; b) a navigation path of the UAV;
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`or c) a maximum angular speed allowable for the UA V or the imaging device, as recited in claim 1.
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`Additionally, the cited disclosure of Lee fails to suggest automatically adjusting the UAV, the
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`carrier, or the imaging device so as to substantially correct the detected deviation from the
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`predetermined position or the predetermined size of the target, wherein the one or more processors,
`
`individually or collectively, make a determination to adjust 1) the UAV, 2) the imaging device, or 3)
`
`both the UA V and the imaging device, wherein said determination is dependent upon a) a navigation
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`path of the UAV; orb) a maximum linear speed allowable for the UAV, as recited in claim 13.
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`Since the combination of Bevirt and Lee fail to disclose all elements of independent
`
`claims 1 and 13, claims 7-12, 15, and 19 are not obvious in view of Bevirt and Lee and
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`withdrawal of this rejection is respectfully requested.
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`Claims 26-30 were rejected under 35 U.S.C. 103 as allegedly being unpatentable over
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`Bevirt in view of Karins et al. (US 2012/0143808 Al).
`
`Claim 26 depends directly upon base claim 22, which recites that the one or more
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`processors, individually or collectively, make a determination to adjust 1) the UAV, 2) the imaging
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`device, or 3) both the UA V and the imaging device, wherein said determination is dependent upon a)
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`number of rotational axis of the imaging device and orientation of said rotational axis relative to the
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`UA V; b) a navigation path of the UA V; or c) a maximum angular speed allowable for the UA V or
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`the imaging device. As previously mentioned, one or more elements of independent claim 22 are
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`missing from Bevirt.
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`Karins fails to cure the deficiencies of Bevirt. Karins discloses an apparatus, system, and
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`method for identifying a target object (Karins, Abstract). Karins fails to teach that the one or
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`more processors, individually or collectively, make a determination to adjust 1) the UAV, 2) the
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`imaging device, or 3) both the UAV and the imaging device, wherein said determination is dependent
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`upon a) number of rotational axis of the imaging device and orientation of said rotational axis
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`relative to the UAV; b) a navigation path of the UAV; or c) a maximum angular speed allowable for
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`the UA V or the imaging device, as recited in claim 22. Since the combination of Bevirt and
`
`Karins fail to disclose all elements of claim 22, claim 26 is not obvious in view of Bevirt and
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`Karins.
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`Independent claim 27 is directed to a system for controlling an unmanned aerial vehicle.
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`Claim 27 as amended recites "a transmitter for providing ... user's input on allocation of control
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`over a tracking process between the user and an onboard processing system of the UAV." This
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`element and/or others are missing from Bevirt and Karins.
`
`Bevirt discloses a system for tracking and video surveillance using an aerial videographic
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`platform (Bevirt, Abstract). The platform may allow a user to "select from a variety of
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`operational modes" (Bevirt, paragraph [0015]). The operational modes may relate to recording
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`from prescribed positions or relative to the OoI location, or relative to a fixed reference location
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`(Bevirt, paragraph [0015]). Karins discloses an apparatus, system, and method for identifying a
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`target object (abstract). Nothing in the cited disclosure of Bevirt nor Karins teaches or suggests a
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`system that apparatus that allows for a user's input on allocation of control over a tracking
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`process between the user and an onboard processing system of the UAV (emphasis added).
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`Accordingly, one or more elements of independent claim 27 are missing from both Bevirt and
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`Karins. Therefore, claim 27 and claims 28-30 which are dependent on claim 27 are not obvious
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`over Bevirt in view of Karins.
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`Accordingly, claims 26-30 are not obvious in light of the cited references. A request is
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`respectfully made for withdrawal of this rejection.
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`7237480.DOC
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`-13-
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`Atty. Docket No.: 45236-734.301
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`Yuneec Exhibit 1006 Page 13
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`
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`Serial No. 14/471,954
`Non-Final Office Action Mailed On January 5, 2015
`Supplemental Amendment And Response To Non-Final Office Action Filed May 7, 2015
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`CONCLUSION
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`Applicants believe that the application is in condition for allowance and respectfully
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`solicit the Examiner to expedite prosecution of this patent application to issuance. Should the
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`Examiner have any questions, the Examiner is encouraged to telephone the undersigned.
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`The Commissioner is authorized to charge any additional fees which may be required,
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`including petition fees and extension of time fees, to Deposit Account No. 23-2415 (Docket No.
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`45236-734.301).
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`Respectfully submitted,
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`WILSON SONSINI GOODRICH & ROSATI
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`By: _ _ (_f_..__.---_· - - - -
`Elaine Kim, Reg. No. 57,613
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`Dated: May 7, 2015
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`650 Page Mill Road
`Palo Alto, CA 94304-1050
`Direct Dial: (650) 565-3808
`Customer No. 021971
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`7237480.DOC
`
`Atty. Docket No.: 45236-734.301
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`-14-
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`Yuneec Exhibit 1006 Page 14