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Matches 1 - 50 out of 4,319

Document Document Title
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/2018/224565A2
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 ...  
WO/2018/158511A1
The present invention relates to a redundant and dissimilar system (10) for monitoring the status of contactors (22) of an aircraft control stick (20). This monitoring system (10) comprises at least one electrical power source (2), at le...  
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/2018/156618A1
The present invention discloses improvements to mechanical and electro-mechanical force simulators for aircraft pilot controllers, and particularly foot-actuated controllers. In particular, the invention replaces conventional foot-actuat...  
WO/2018/156335A2
Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distribut...  
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/2018/156139A1
A computer is programmed to determine a trajectory of a moving target based on data from one or more vehicle sensors. The computer is programmed to deploy an aerial drone from the vehicle to track the moving target based on the determine...  
WO/2018/156335A3
Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distribut...  
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/2018/142246A1
A backup actuation control unit for controlling an actuator dedicated to a given surface. The backup actuation control unit comprises a processing unit operatively connected to one of a flight control computer and a backup flight control...  
WO/2018/135332A1
[Problem] To provide a technology capable of accurately controlling the orientation of a flying object. [Solution] This orientation control device is equipped with a control unit. The control unit controls the orientation of the flying o...  
WO/2018/132096A1
An aircraft passenger cabin airflow metering apparatus and system is provided. The apparatus includes a blowout disc designed to release at a predetermined air pressure differential on opposite sides of the blowout disc. The blowout disc...  
WO/2018/132291A1
The subject matter of this specification can be embodied in, among other things, a motion control apparatus that includes a brushless DC motor to actuate a mechanical output based on a collection of phase power signals, a collection of f...  
WO/2018/123747A1
A novel system enabling simpler drone maneuvering is provided. A drone maneuvering system 1 includes a drone 30 and a maneuvering signal transmitter set 10. The maneuvering signal transmitter set 10 includes a first transmitter 100 that ...  
WO/2018/114544A1
A movable flight surface for an aircraft, comprising: – an envelope (20) mounted so as to pivot on an articulation axis (21) having at least one end projecting from the envelope, – at least one electric motor (51) which is mounted in...  
WO/2018/114545A1
Electromechanical device for actuating a movable flight surface (11, 12) having an envelope (20) articulated to an aircraft structure about an axis of rotation (21), comprising: – at least two electric motors (51) for rotating the enve...  
WO/2018/118070A1
A set of commands for each of a plurality of actuators to alter an aircraft's state responsive to one or more inputs is produced. The set of commands is provided to fewer than all actuators comprising the plurality of actuators.  
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/2018/110634A1
A problem to be addressed by the present invention is to provide a flight management system and flight management method for actively managing the flight of an unmanned aerial vehicle. Provided is a flight management system, etc., of an ...  
WO/2018/108943A1
A control system for use in a vehicle configurable for air use or road use, the vehicle comprising moveable control surfaces for controlling operation of the vehicle in air use, wherein the system comprises: a pedal arrangement of three ...  

Matches 1 - 50 out of 4,319