| Document |
Document Title |
|
WO/2018/167472A1 |
The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization unit...
|
|
WO/2018/169154A1 |
The present invention relates to a personal imaging system using a flying object and, in particular, to a personal imaging system which can acquire an image while following a user by using a balloon-type flying object. In the present inv...
|
|
WO/2018/168564A1 |
[Problem] To provide a simple method and a simple device capable of accurately measuring the water depth of a field, in particular, the entirety of a rice field. [Solution] By flying, in the air above a field, a drone (unmanned flying bo...
|
|
WO/2018/163298A1 |
A control device may comprise a control unit that controls a heating unit that heats an optical member provided forward of an image sensor. The control unit may cause the heating unit to heat the optical member when an imaging device is ...
|
|
WO/2018/164426A1 |
The present invention relates to a method for detecting a porphyry copper ore body by using hyperspectral imaging of malachite, the method comprising the steps of: obtaining hyperspectral image data of an alteration zone indicated by alt...
|
|
WO/2018/163692A1 |
This heat radiator for an aircraft cools a heat source mounted on the aircraft and is provided with a heat radiation section (3) having recesses or protrusions formed on the surface thereof which comes in contact with a main stream, the ...
|
|
WO/2018/163571A1 |
An information-processing device operating in an imaging device mounted in a mobile entity, which, when image capture by the imaging device fails, notifies the mobile entity to the effect that image capture has failed.
|
|
WO/2018/163699A1 |
[Problem] To provide a control system for a flight vehicle that causes the flight vehicle to fly autonomously without the use of GPS and without storing flight routes, and a control device for the same. [Solution] A control system 2 for ...
|
|
WO/2018/157633A1 |
Provided is a shock absorber (100), comprising a connecting portion (102) and buffering portions (101) respectively located on either end of the connecting portion, wherein the cross-sectional size of the shock absorber gradually decreas...
|
|
WO/2018/158927A1 |
The present invention highly precisely estimates the shape of an object irrespective of whether there are variations in the altitude of the shape of the object, and avoids a collision between the object and a flying vehicle during flight...
|
|
WO/2018/152770A1 |
A cradle head assembly (100), comprising: a fixed bracket (110); at least two mounting seats (130) disposed opposite to the fixed bracket (110) and disposed at intervals; a shock absorbing mechanism (120) connected between the fixed brac...
|
|
WO/2018/152909A1 |
A cradle head device (100) and an unmanned aerial vehicle (300) using the same. The unmanned aerial vehicle (300) comprises a fuselage (200), and the cradle head device (100) is fixed to the fuselage (200). The cradle head device (100) c...
|
|
WO/2018/155700A1 |
The present invention addresses the problem of providing a flight management system for managing flight plans of flying objects that fly between ports. This flight management system which is equipped with multiple port management devices...
|
|
WO/2018/152783A1 |
Disclosed is an image processing method, applied in an aircraft (100). The aircraft (100) is provided with an imaging device (10). The processing method comprises the steps of: (S22) controlling the imaging device (10) to perform imaging...
|
|
WO/2018/152785A1 |
Disclosed is an unmanned aerial vehicle (100), comprising a body (10) and a battery module (40). The body (10) comprises a bottom portion (11) facing the ground. The battery module (40) comprises a battery having a top portion (41) oppos...
|
|
WO/2018/152943A1 |
Provided are a motor (100), a cloud platform (300) and an unmanned aerial vehicle. The motor comprises a first connection terminal and a second connection terminal. The first connection terminal comprises a circuit board (13) comprising ...
|
|
WO/2018/148899A1 |
Provided are a three-axis mount and a control method thereof. The three-axis mount (1) comprises three sets of shaft arm components (11, 12, 13). Each set of the shaft arm components comprises a motor component and a rotating arm compone...
|
|
WO/2018/150917A1 |
Provided are a steered object, a moving device, an imaging device, a movement control method, a movement assist method, a movement control program, and a movement assist program with which it is possible to perform an appropriate process...
|
|
WO/2018/149465A1 |
The attachment of a projector under the cowling of a turbofan engine (110) of a modern commercial aircraft (100) allows the illumination of the underside (130) and of the sides (132) of the aircraft fuselage and also of the underside (13...
|
|
WO/2018/150492A1 |
To enable an unmanned aerial vehicle to easily fly to a desired position while checking an aerial image, is desired. This image display method in an image display system for displaying an image based on an aerial image captured by a flyi...
|
|
WO/2018/149182A1 |
A pan-tilt and an unmanned aerial vehicle. The pan-tilt comprises: a first circular member (60); a second circular member (66), the second circular member (66) being fitted outside the first circular member (60); a rotational member (70)...
|
|
WO/2018/145261A1 |
A multifunctional camera, comprising a connector (1), at least two rotation members (2) respectively disposed on the connector, and a rotation member driving mechanism. Each rotation member is provided with a camera body (100) correspond...
|
|
WO/2018/147522A1 |
The present invention relates to a flying lighting device having a heat dissipation part provided in a gimbal, the device being capable of: minimizing a region, at which light has not been emitted because of shadow, by emitting light abo...
|
|
WO/2018/142470A1 |
[Problem] To provide a camera control device that enables a photographer to intuitively and easily control a camera mounted to a drone. [Solution] This camera control device 9 transmits a camera control signal to a panning-direction driv...
|
|
WO/2018/137131A1 |
Systems, apparatuses and methods for indicating a moveable device such as an UAV (20) are disclosed herein. The present technology provides an illumination system (200, 200a, 300, 400, 500) having a light source (201, 201a, 301, 601) and...
|
|
WO/2018/134926A1 |
An optical device includes a lens barrel for storing a lens that moves in the optical axis direction. The optical device includes a first guide pole and a second guide pole that control the movement of the lens in the optical axis direct...
|
|
WO/2018/136753A1 |
Indoor mapping and modular control for UAVs and other autonomous vehicles, and associated systems and methods. A representative unmanned aerial vehicle system includes a body, a propulsion system carried by the body, a sensor system carr...
|
|
WO/2018/132990A1 |
A camera mount assembly, and hand-held camera mount-based image capturer. The camera mount assembly (100a, 100b, 100c) comprises a main body (1a, 1b, 1c) and a camera mount support frame (2a, 2b, 2c) connected to the main body (1a, 1b, 1...
|
|
WO/2018/135114A1 |
[Problem] To provide a technology capable of accurately controlling the orientation of an item being held. [Solution] This orientation control device is equipped with a control unit. The control unit controls the orientation of an item t...
|
|
WO/2018/133393A1 |
An aircraft and a pan-tilt limiting device (10) thereof. The pan-tilt limiting device (10) comprises a rotor (13), a rotating shaft (14), a stator (15), and a limiting member (16). A limiting portion (141) is provided on the outer side w...
|
|
WO/2018/132038A1 |
The utility model relates to devices for monitoring aircraft flight parameters and can be used for video recording emergency situations in flight and analyzing such situations. The claimed device for generating an aircraft state of emerg...
|
|
WO/2018/132167A1 |
Example wirelessly powered unmanned aerial vehicles and tracks for providing wireless power are described herein. An example apparatus includes a track section having a transmitter coil to generate an alternating magnetic field and an un...
|
|
WO/2018/119803A1 |
Provided is a gimbal load installation assembly (12) used for being slideably installed on a gimbal support (20), so as to adjust the centre of gravity of a load installed on the gimbal load installation assembly (12). The gimbal load in...
|
|
WO/2018/119768A1 |
A connection device, a cradle head assembly provided with the connection device and a capture assembly, comprising: a capture device (300) and a cradle head (20) which is used for carrying the capture assembly; the cradle head assembly c...
|
|
WO/2018/124688A1 |
A drone control device for collision avoidance, according to an embodiment, comprises: a driving unit for driving a rotor blade of a drone; a sensor unit including an omnidirectional camera for acquiring an omnidirectional image by photo...
|
|
WO/2018/119555A1 |
Disclosed is an unmanned aerial vehicle (1), comprising an obstacle avoidance device (2). The obstacle avoidance device (2) is provided with an image sensor (21), and the axial direction (20) of the image sensor (21) can be arranged in a...
|
|
WO/2018/124662A1 |
An electronic device is disclosed and includes a display, a wireless communication circuit configured to transmit or receive data, a processor, and a memory electrically connected with the processor. The memory stores instructions, which...
|
|
WO/2018/119802A1 |
Provided is a gimbal frame (20) used for installing a load. The gimbal frame (20) comprises a guide rod (22), and a centre of gravity adjusting and locking mechanism (5) installed on the guide rod (22). The centre of gravity adjusting an...
|
|
WO/2018/113202A1 |
A detachable pan-tilt connection device (300) and an unmanned aerial vehicle (100). The detachable pan-tilt connection device (300) comprises: an alignment assembly, being used for aligning a circuit connection terminal of the unmanned a...
|
|
WO/2018/112907A1 |
Disclosed is a gimbal structure, comprising a gimbal support (1) and a reflective mirror (5) arranged on the gimbal support (1), wherein the gimbal support (1) is used for fixing a photographing device (6) and enables the photographing d...
|
|
WO/2018/113134A1 |
A multi-rotor unmanned aerial vehicle (100), comprising a main vehicle assembly (10) and a plurality of rotor assemblies (20). Each rotor assembly (20) comprises a servomotor (21), a connecting arm (22), and a rotor unit (23). The main v...
|
|
WO/2018/113519A1 |
A pan-tilt (1) for an unmanned aerial vehicle, and an unmanned aerial vehicle. The pan-tilt (1) for an unmanned aerial vehicle comprises a first fixed device used for being fixedly mounted on an unmanned aerial vehicle body, a first conn...
|
|
WO/2018/117627A1 |
An unmanned aerial vehicle (UAV) is provided. The UAV includes a first guard grill, a second guard grill configured to be removably combined with the first guard grill and form an external structure and an inner space of the UAV with the...
|
|
WO/2018/110382A1 |
Provided is a flying device having: an acquisition unit that acquires communication quality information in which position information indicating a position and the communication quality at the position indicated by the position informati...
|
|
WO/2018/110088A1 |
An unmanned aircraft 1 according to one embodiment of the present invention is able to properly make an emergency landing in case of an abnormality. The unmanned aircraft 1 is configured as a multicopter which flies with the lift and thr...
|
|
WO/2018/107416A1 |
A manually operable mechanism for mechanically and electrically connecting parts of an unmanned aerial vehicle (UAV) comprises a first engaging means (20) associated with a first part of the UAV including at least one first electrical co...
|
|
WO/2018/107330A1 |
The systems, methods, and devices related to the control and operation of a carrier for supporting a payload. In one aspect, a carrier may comprise: a stator configured to be coupled to a base support, said stator comprising a spherical ...
|
|
WO/2018/111488A1 |
An aircraft including a wing system, a plurality of control surfaces, a camera mounted on a camera pod, and a control system. The camera pod is configured to vary the orientation of the camera field of view only in yaw, relative to the a...
|
|
WO/2018/107337A1 |
A pan-tilt (100), comprising a driving mechanism (40). The driving mechanism (40) comprises a rotor assembly (43) and a stator (41); the rotor assembly (43) comprises an installing member (431) used for bearing an external load, and a dr...
|
|
WO/2018/111346A1 |
A device is provided for controlling fluid flow over a window of a movable optical instrument housing. The device includes a generally annular body having an inner peripheral edge configured to correspond to a peripheral edge of the wind...
|
