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Matches 1 - 50 out of 4,485

Document Document Title
WO/2019/099538A1
Systems and aircraft are provided. An avionics system includes a storage device and one or more data processors. The storage device stores instructions for monitoring an actual performance of the aircraft. The one or more data processors...  
WO/2019/097919A1
Provided is an electric actuator device that has a simple structure and that makes it easy to release the mechanical connection between a rudder surface and an aircraft body, such connection due to the electric actuator. An electric actu...  
WO/2019/092708A1
A control system and a method are adapted to restrain turbulence induced yaw or side movements of an airborne vehicle (AV) that has at least two electrical motors, the motors are disposed one on the left and one on the right side of a lo...  
WO/2019/093198A1
The present invention avoids a collision with a flying body operated by another party, on the basis of the classification of said flying body. A detection unit detects the presence of another flying body (10A) within a prescribed range f...  
WO/2019/093504A1
Provided is a method for performing roofing surveys without having people climb onto roofs. First, an application installed on a terminal 130 is launch, the user logs in as necessary, and then inputs instructions for new image capture (S...  
WO/2019/087891A1
The objective of the present invention is to enable piloting support for a pilot of an aircraft to be performed from a remote location. A server device (20) functions as a control platform for controlling the flight of an aircraft (10). ...  
WO/2019/080101A1
Disclosed are information receiving and sending methods and apparatuses, an unmanned aerial vehicle, a network device, and a computer readable storage medium. The information receiving method comprises: reporting the identifier (ID) of a...  
WO/2019/082924A1
According to the present invention, piloting assistance for a pilot in an aircraft can be easily provided from a remote location. A server device (20) preferentially provides an assistance terminal (50) with any one among a captured imag...  
WO/2019/077963A1
The present invention comprises: a fuselage frame (10); a thrust unit (20) for generating thrust for flying; an airflow sensor (30) for acquiring airflow information relating to the surrounding airflow; and a control device (40) for cont...  
WO/2019/077694A1
The present invention lessens delay in flight control against wind change. This unmanned aircraft control system (1) includes: a first unmanned aircraft (10); a second unmanned aircraft (10) which flies near the first unmanned aircraft w...  
WO/2019/076341A1
A flap retraction and releasing apparatus (100), comprising: a support base (3), which is arranged along an air flow and can be fixedly connected to a fixed trailing edge of an aircraft wing; a first rotating shaft (6), which is rotatabl...  
WO/2019/073984A1
[Problem] The purpose of the present invention is to provide a method for efficiently shading the whole of a fixed tract of land having no roofing, supports for a roof, or the like, such as schoolyard or a track and field stadium. [Solut...  
WO/2019/073601A1
The present invention meets flying distance and flying time requirements while effecting safe flight for an unmanned flying body. This unmanned flying body comprises: a thrust generating device; a flight control device that controls the ...  
WO/2019/069287A1
A stability and command augmentation system (20) for controlling an aircraft (1), comprising: a first member (19) moveable by a pilot input device (10, 11, 15) to a first position defining a first input (xi); a second member (22) moveabl...  
WO/2019/064329A1
The present invention accurately and efficiently causes an unmanned moving body to land in a determined location. There is used a control unit (25) that is a CPU for controlling a data storage unit (24) that stores data and controlling t...  
WO/2019/058991A1
Provided is a communication relay device with which it is possible to stably achieve a three-dimensional network, such as 5G mobile communication, across a wide area, and to reduce energy consumption. The communication relay device compr...  
WO/2019/058623A1
A supply plan device 10 calculates a first route supply point on a movement route at which the supply of a chemical agent is required, a second route supply point on the movement route closer to a supply area than the first route supply ...  
WO/2019/059394A1
A compact unmanned mobile body capable of carrying a package with reduced risk during package transportation, and a package collection and delivery method involving the use of the compact unmanned mobile body, wherein the compact unmanne...  
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...  

Matches 1 - 50 out of 4,485