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WO/2019/140522A1 |
The present disclosure provides methods and systems for providing vertical flight guidance for an aircraft. Vertical flight guidance for the aircraft is provided by an aircraft computer in an altitude capture mode for commanding the airc...
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WO/2019/139172A1 |
The purpose of the present invention is to effectively use a small unmanned aircraft in all fields in which research and development are advancing. An information processing system that includes a drone 1 having a drive unit 11 for movin...
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WO/2019/139654A1 |
There is provided a dual rack and pinion rotational inerter system (500) for damping movement (694) of a flight control surface (122) of an aircraft (100). The system (500) has a flexible holding structure (506) disposed between the flig...
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WO/2019/138466A1 |
In order to assist an operator of an unmanned aircraft while limiting power consumption, an operation information acquisition means (101) of this unmanned aircraft control system (S) acquires operation information pertaining to at least ...
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WO/2019/139653A1 |
There is provided a translational inerter assembly (500) for damping movement (606) of a flight control surface (122) of an aircraft (100). The assembly (500) has a press fit element (510) fixedly disposed within a first end (502a) of th...
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WO/2019/130973A1 |
This work site management system is provided with an image data acquisition unit which acquires image data of an unmanned vehicle that has stopped in the work site due to occurrence of abnormality, the image data being captured by an ima...
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WO/2019/122807A1 |
Aircraft control systems to enable shared input controls. A single inceptor may provide outputs to control both land-based aircraft controls and air-based aircraft controls to reduce the number of inceptors required. In an example a side...
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WO/2019/110782A1 |
The invention relates to a mechanical no-back mechanism for use in an aircraft, where the use in question can be part of a flight control system. The no-back mechanism comprises at least one constant brake, at least one main brake and at...
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WO/2019/107047A1 |
The present invention appropriately restricts a flight airspace for a flying object. A setting unit (202) sets a flight restriction airspace for a flying object (10) on the basis of ground attribute conditions related to ground attribute...
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WO/2019/104421A1 |
A system and a method for improving a stall margin of an aircraft during a climb phase of flight are disclosed. In one embodiment, the method comprises using data indicative of a phase of flight of the aircraft and data indicative of an ...
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WO/2019/106714A1 |
Provided are a flight control device, a flight control method, and the like for measuring the distance between the body of an aircraft and a target element during flight and controlling the distance in accordance with the measured value....
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WO/2019/100149A1 |
A system and method for actuating one or more high-lift flight control surfaces of an aircraft are disclosed. The system comprises actuators operatively coupled between a driveline and one or more high-lift flight control surfaces associ...
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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...
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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...
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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...
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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...
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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...
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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). ...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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