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Matches 1 - 50 out of 4,405

Document Document Title
WO/2019/054029A1
An acquisition unit acquires: a flight plan that states a first flight condition; and information that indicates a time limit set for a location on a path on which an aerial vehicle flies. An arrival determination unit determines whether...  
WO/2019/054027A1
An acquiring unit of the present invention acquires a flight plan containing first flight conditions. A setting unit sets a risk level for airspace in which an aircraft is flying. A determining unit determines second flight conditions. A...  
WO/2019/054028A1
An acquisition unit acquires, by communicating with a server device, a flight plan that states a first flight condition. A state determination unit determines the state of communication. A condition determination unit determines a second...  
WO/2019/051432A1
Enclosures for facilitating activities in space, and associated systems and methods, are disclosed. A representative system includes a spacecraft having an enclosed interior volume (which can be formed by an inflatable membrane) and one ...  
WO/2019/049313A1
[Problem] To provide an aerial vehicle having improved responsiveness during transportation. [Solution] An aerial vehicle 1 includes: a fixed rotor 20b (20) that supports a first rotary wing 50b so as to allow rotation thereof; a movable...  
WO/2019/049197A1
An objective of the present invention is to provide an aircraft that can fly more reliably in a desired position. This aircraft is characterized by comprising an image capture means for capturing an image of the periphery of the aircraft...  
WO/2019/043645A1
A method and a system are disclosed for determining an estimation of an anemometric parameter of an aircraft, the anemometric parameter selected from a group comprising at least one of an angle of attack, a sideslip angle and a calibrate...  
WO/2019/044125A1
This flying body comprises: a fuselage; a canopy capable of adjusting the speed of a fall when falling; a brake cord having one end connected to the canopy; a winding device (20) which is provided on the fuselage and allows the other end...  
WO/2019/038927A1
This flight vehicle is capable of hovering in a desired position more reliably, and is characterized by being provided with: a determination means for determining whether the flight vehicle is to be caused to hover or not; an image captu...  
WO/2019/037452A1
A rudder device and an aircraft having same. The rudder device comprises: a rudder surface (10) connected to a stabilizing surface (100) by means of a first pivot shaft (11), the first pivot shaft (11) being parallel to an axial directio...  
WO/2019/030820A1
In order to more reliably land a flying vehicle at a desired location, the flying vehicle is provided with: a determination means which determines whether the flying vehicle is taking off and ascending from a take-off point, or is descen...  
WO/2019/026179A1
A wireless communication device installed in a drone transmits information pertaining to the drone, a relay that flies at a first altitude between the altitude at which the drone can fly and the altitude of a communication satellite rece...  
WO/2019/024401A1
A flap/slat control lever (200) and a method for operating the lever. The lever comprises: a first displacement sensor (204), used to detect displacement of the flap/slat control lever and to generate a first displacement detection signa...  
WO/2019/023322A1
A method, preferably including: sampling inputs, determining aircraft conditions, and/or acting based on the aircraft conditions. A method, preferably including: sampling inputs, determining input reliability, determining guidance, and/o...  
WO/2019/021915A1
A portable electronic instrument according to one aspect of the present invention is connected to a flying device. The portable electronic instrument is provided with a communication unit which communicates with the flying device, and a ...  
WO/2019/023527A1
An example embodiment includes a plurality of flight modules including a primary flight module and a secondary flight module. The embodiment includes a CAN controller, a second CAN controller, a first CAN bus configured to transmit prima...  
WO/2019/016930A1
The present invention determines, with a high degree of accuracy, the magnitude of influence exerted by wind on a moving body from information acquired from the moving body. This data processing device is provided with: an acceleration a...  
WO/2019/017325A1
This aircraft steering system (10A) is provided with: a first actuator (21) mounted to a wing main body (11); a horn arm (13) which transmits an output of the first actuator (21) to a steering surface (12); and a second actuator (22) whi...  
WO/2019/013151A1
The present invention addresses the problem of providing a method for setting a flight altitude, and an unmanned aerial vehicle system, with which a flight altitude in a flight plan can be set efficiently in accordance with undulations a...  
WO/2019/008669A1
In the present invention, landing location candidates are determined that are within the range within which an aircraft (3) can travel and are near the route of a vehicle (30A), and a landing location for the aircraft (3) is selected fro...  
WO/2019/009229A1
The objective of the present invention is to provide a flight control device capable of efficiently implementing a special autonomous flight operation, and an unmanned aerial vehicle provided therewith. This objective is achieved by mean...  
WO/2019/003492A1
The present invention addresses the problem of suitably projecting an image to a target position. A control device (10) controls a mobile body (1) that is provided with a projection unit (3). The control device (10) is provided with: a p...  
WO/2019/005137A1
A monitoring system (5, 205) for an aircraft (10) has sensors (20, 30) that are used to sense the air movement around the aircraft. The monitoring system may use information from the sensors to estimate the effects of the air movement on...  
WO/2018/230680A1
This drone coordination device comprises: an acquisition unit that acquires an action plan from an automatic driving vehicle; and a determination unit for determining a flight plan for a drone, including the area in which the drone is to...  
WO/2018/229761A1
According to the presently disclosed subject matter there is provided an in-flight UAV retrieval system mountable on an aircraft and configured to execute a UAV retrieval process for retrieving one or more in-flight UAVs into the aircraft.  
WO/2018/232196A1
The present disclosure relates to aircraft and aircraft flight control systems, methods, and apparatuses. A condition-aware aircraft configured to make in-flight decisions autonomously, based on the most up-to-date information, to perfor...  
WO/2018/225112A1
[Problem] To provide an aerial vehicle wherein the flight efficiency can be improved. [Solution] An aerial vehicle according to the present invention relates in particular to a aerial vehicle having a loading section whereon a payload an...  
WO/2018/224565A3
The present invention discloses a method and flight controller for controlling an aircraft, comprising the following step: - determining the pitch control input δE for at least one pitch moment generator element, based on the lift contr...  
WO/2018/224565A2
The present invention discloses a method and flight controller for controlling an aircraft, comprising the following step: - determining the pitch control input δE for at least one pitch moment generator element, based on the lift contr...  
WO/2018/218370A1
Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the w...  
WO/2018/221022A1
When measuring antenna radiation patterns in an environment in which radio waves are reflected, it is difficult to measure with high precision due to the multipath effect. This radio wave measurement system is provided with: a flying bod...  
WO/2018/220539A1
The present disclosure relates to a method of assessing the presence of an electrical, electronic and/or mechanical fault in an electromechanical linear actuator (1), said electromechanical linear actuator (1) comprising a containment st...  
WO/2018/220996A1
When measuring antenna radiation patterns in an environment in which radio waves are reflected, it is difficult to measure with high precision due to the multipath effect. This radio wave measurement system is provided with: a flying bod...  
WO/2018/216532A1
While a flight vehicle that has an antenna and flies in the stratosphere in order to provide a stratosphere platform has been known, it is desirable to provide a technology for controlling the antenna appropriately in accordance with the...  
WO/2018/215649A1
The invention relates to a flight control system (1) for actuating a control surface (2) of an aircraft, comprising: a plurality of actuators (3) for the redundant actuation of a control surface (2) of the aircraft; actuator control elec...  
WO/2018/211777A1
[Problem] To make it possible to more appropriately control the flight of a UAV. [Solution] Provided is a control device comprising: an identification unit that identifies a marker provided on the ground, on the basis of information obta...  
WO/2018/207678A1
This unmanned aerial vehicle moves in midair and is capable of performing fluorescent X-ray analysis of a predetermined object of measurement, and is characterized by being provided with: an aerial vehicle main body; a fluorescent X-ray ...  
WO/2018/207612A1
The present invention provides a communication system having excellent robustness and capable of stably building, over a wide region, a three-dimensionally formed network where, in the fifth-generation mobile communication and the like, ...  
WO/2018/203520A1
The purpose of the present invention is to provide: a flight function addition device in which a plurality of rotor units are mounted on an article to be transported and the movement of the rotor units is coordinated, whereby the article...  
WO/2018/195419A1
An actuator for positioning a solar array to track the sun includes a motor and a single-stage cycloidal gearbox operatively coupled to the motor. The single-stage cycloidal gearbox includes a drive shaft rotationally coupled to the moto...  
WO/2018/189848A1
[Problem] To provide a method for controlling the flight of a drone and a program with which the drone performs accurate spraying of a chemical in farmland located in narrow and complicated terrain even when there is no accurate map info...  
WO/2018/190319A1
The flight vehicle (1A) is provided with: a lift-generating member (1110) disposed on an airframe (1201) in a deployable manner; manipulation mechanisms (1111, 1112), which are connected to the lift-generating member (1110) and are for m...  
WO/2018/186256A1
The purpose of the present invention is to provide a highly efficient method for capturing images inside a confined space without the need for direct visual observation by an inspector. Provided is an unmanned aerial vehicle equipped wit...  
WO/2018/186632A1
A flying device of the present invention has one or more wings for performing a relative motion with respect to a body by means of a driving source so as to generate buoyancy, and has one or more air louvers provided at the wings and com...  
WO/2018/184396A1
An electric pedal control device for an aircraft. The device comprises several pedal transmission assemblies. Each of the pedal transmission assemblies comprises a motor (1), an elastic connector (3), a transmission mechanism, an angular...  
WO/2018/180534A1
In order to solve the problem in which a flight vehicle flies only in locations having poor communication quality and retained data cannot necessarily reach the ground, this device communicates with a flight vehicle, wherein the device i...  
WO/2018/167013A1
The invention relates to a device (1) for connecting an end of a first shaft to an end of a second shaft, the end of the first shaft having a radial groove, the device comprising: -a body (2) having a bore (21) into which the end of the ...  
WO/2018/165915A1
A method for planning a waypoint of an unmanned aerial vehicle (200) for an electronic device (100). The method comprises: in a case in a which an electronic device (100) does not establish a communication connection (300) with an unmann...  
WO/2018/164241A1
A rotary connector (1) is provided with: an electrically conductive shaft (2); a bearing (3) which rotatably supports the shaft (2); and a housing (4) in which the bearing (3) is disposed and which includes an electrode portion (11) at a...  
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 ...  

Matches 1 - 50 out of 4,405