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WO/2018/110598A1 |
The objective of the present invention is to provide a device, method, and the like that, when a failure has occurred, and in particular when a failure has occurred in the operation of part of a rotary wing, can control flight in accorda...
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WO/2018/111258A1 |
A computer is programmed to deploy an aerial drone to fly within a specified distance of a first vehicle. The computer is programmed to detect a second vehicle and then activate an aerial drone light.
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WO/2018/106384A1 |
A magnetic spring input device is disclosed. In various embodiments, an input device as disclosed includes a manual input structure movably coupled to a base assembly; and a non-stationary magnet fixedly coupled to the manual input struc...
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WO/2018/105576A1 |
Provided is a flying device that flies by external control, the flying device having: an identification unit which identifies the communication quality of a first wireless communication channel used for transmission of data to a control ...
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WO/2018/100494A1 |
The aircraft control systems and methods disclosed herein are configured to detect a residual error associated with a flight control computer of an aircraft and mitigate the effect(s) of such residual error in order to maintain safe oper...
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WO/2018/095934A1 |
An actuator (10) for at least one movable flight surface (3.1, 3.2, 4.1, 4.2) of an aircraft, comprising at least two members (30) for actuating the movable flight surface between two limit positions and a motor (20) linked to the actuat...
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WO/2018/094312A1 |
An unmanned vehicle is configured to deliver packages or other payloads includes a first sensor, a second sensor, a third sensor, and a control circuit. The first sensor is configured to sense infrared energy, and the second sensor is co...
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WO/2018/091475A1 |
The invention relates to an electrohydraulic module (1) for driving at least one component of an aircraft, in particular an airplane, wherein the electrohydraulic module (1) comprises at least one electric motor (2) and at least one comp...
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WO/2018/087353A1 |
The invention relates to a device (1) for encoding information between a plurality of normally closed switches (P1...Pn) arranged on an operating lever (2) and a control device (9), said switches being connected in series between a volta...
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WO/2018/083942A1 |
[Problem] To provide a framework by which the safety of an autonomous mobile device in an emergency situation can be further improved. [Solution] A circuit provided with: a notification unit for notifying a base station of operable time ...
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WO/2018/078863A1 |
[Problem] To provide a drone control system that enables a drone to move to a position where an objective can be achieved and carry out an action according to the objective. [Solution] A drone control system 1 controls a drone 10 that ca...
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WO/2018/080344A1 |
The invention relates to highly manoeuvrable aircraft with a multi-functional control system. The present aircraft comprises an integrated control system (ICS) which includes a computing unit connected by inputs and outputs to flight con...
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WO/2018/069637A1 |
The invention concerns the field of powering and controlling electrical actuators (32A, 32B, 32C) installed in an aircraft. In particular, it concerns a system (31) for powering and controlling a plurality of electrically controlled actu...
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WO/2018/070486A1 |
One purpose of the present invention is to provide a novel and simple-structured autonomous attitude control system for a mobile body (for example, an unmanned small-sized aircraft). Another purpose of the present invention is to provide...
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WO/2018/068193A1 |
Provided are a control method, a control device, a flight control system, and a multi-rotor unmanned aerial vehicle. The control method comprises: controlling a multi-rotor unmanned aerial vehicle to fly toward a target location (210); d...
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WO/2018/066043A1 |
Provided is a delivery rotary-wing aircraft capable of stably landing on a destination free of influence from an updraft occurring in a region, such as tall buildings. This rotary-wing aircraft comprising a plurality of rotary wings, a c...
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WO/2018/066918A2 |
A flapping flight device according to the present invention is a flight device having at least one wing on each of the left and right sides of a fuselage so as to make a relative movement with regard to the fuselage by means of a driving...
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WO/2018/062336A1 |
This flight control device 10 comprises a route information acquisition unit 11, a position identification unit 12, an environmental information acquisition unit 13, and a flight control unit 14. The route information acquisition unit 11...
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WO/2018/054105A1 |
A buckled beam-based bi-stable state electromagnetic steering engine and a control method. The steering engine comprises an electromagnetic driving device, a buckled beam control device, and a rudder which is connected to the buckled bea...
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WO/2018/053862A1 |
A power system configuration method, the method comprising: acquiring environmental information of an environment where an unmanned aerial vehicle (100) is located; and determining, according to the environmental information, a matched p...
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WO/2018/056498A1 |
The present invention relates to a transmission line electromagnetic field and an instantaneous inspection image acquisition device using an unmanned aerial vehicle, and there is provided an image acquisition device and method comprising...
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WO/2018/050868A1 |
The invention relates to a device and to a method for performing open -and closed -control of n actuators An (101 ), n = 1, 2,..., N, where N ≥ 1, which drive aerodynamic control surfaces (102) of an aircraft. The proposed device compr...
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WO/2018/050866A1 |
The invention relates to a device and a method for reducing gust loads acting on an aircraft. The aircraft has at least one aerodynamic control surface (101) which can be moved by at least one actuator (102), and a flight control system ...
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WO/2018/048706A1 |
In some embodiments, methods and systems of dispensing an insecticide to defend a crop-containing area against crop-damaging pests include an unmanned vehicle having a sensor that detects a crop-damaging pest in the crop-containing area ...
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WO/2018/042676A1 |
The purpose of the present invention is to make the flight time of an unmanned flying body longer. This unmanned flying body comprises: a plurality of rotary blades; a plurality of control devices connected to the rotary blades; and a fl...
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WO/2018/043116A1 |
To provide a small flying body in which it is possible to mitigate impact when the flying body falls and collides with the ground, etc. A small aircraft that has an airbag device and a maximum length of 2 m and that is capable of flying ...
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WO/2018/037796A1 |
This flight device is provided with a base body, thrusters, an attitude detection unit, an abnormality detection unit, and an attitude control unit. The plurality of thrusters are provided to the base body, and are provided with propelle...
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WO/2018/034018A1 |
The present invention provides a novel system enabling a safer operation of a moving body. This moving body operating system (1) of the present invention includes a moving body (11), a plurality of operation signal transmitters (12A, 12B...
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WO/2018/032420A1 |
A method and system for adjusting a flight altitude according to a wind force value, the method comprising the following steps: detecting a wind force value of an unmanned aerial vehicle (S101); determining whether the wind force value i...
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WO/2018/034033A1 |
To provide a device for communication and control for a small unmanned aircraft and a method therefor. A converter module 10 enables communication between a drone 2 and an information processing terminal 4 and includes a communication me...
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WO/2018/020744A1 |
The present invention provides a new system which makes simpler operation of a moving object possible. The moving object operation system according to the present invention includes a moving object and an operation signal transmitter for...
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WO/2018/020853A1 |
The purpose of the present invention is to provide a novel system which makes possible easier control of a mobile body. This mobile body control system (1) comprises a mobile body (20) and a control signal transmission device (10) which ...
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WO/2018/020607A1 |
[Problem] To provide an unmanned aircraft control system, an unmanned aircraft control method, and an unmanned aircraft control program that are beneficial when applied to control of unmanned aircraft, particularly flying drones. [Soluti...
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WO/2018/015022A1 |
The invention relates to a hydraulic flight control actuator, comprising a piston-cylinder device, which has a piston and a cylinder, and comprising a double seal device, which has at least one primary seal (1) and at least one piston ri...
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WO/2018/015719A1 |
A control system (200) using fixed point computation avoids overflow conditions by limiting the internal quantities ensuring that contributing calculations from various parts of the control loop never add up to an overflow. Various parts...
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WO/2018/010130A1 |
A method for operating a motor controller(302),the method may comprise: obtaining an electrical signal via a port (302-1) on the motor controller, wherein the port (302-1) is configured to be electrically connected to a motor (304); and ...
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WO/2018/008388A1 |
The present disclosure relates to an information processing device and an information processing method which make it possible for a flying object to be guided appropriately to a target object even in the presence of a semi-transparent s...
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WO/2018/007010A1 |
The invention relates to a high-lift system comprising means for actuating a wingtip and/or a winglet of the wing of an aircraft between a flight configuration and a ground configuration, comprising at least one drive unit which can be c...
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WO/2018/008675A1 |
Provided are a gas detection system and a gas detection method utilizing a plurality of aerial vehicles, which enable precise detection in a short time. The gas detection system includes: a sending aerial vehicle in which a light-emittin...
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WO/2018/002799A1 |
The present disclosure provides methods and system for controlling the operation of an aircraft aileron which comprises an inboard portion and an outboard portion. A velocity of the aircraft is determined. Then, based on the velocity of ...
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WO/2018/000083A1 |
A control bar stopper includes a stopper body having a sleeved line receiving slip groove that allows sleeved line slippage. The stopper body has an underlying control bar bumper. A brake body is provided having a sleeved line receiving ...
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WO/2018/005524A1 |
Systems and methods for deploying adjacent trailing edge flaps that are part of different flap assemblies of different stiffnesses are disclosed. An exemplary method comprises: deploying a first flap of a first flap assembly having a fir...
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WO/2018/003080A1 |
[Problem] To provide an insecticidal device balance adjustment system, an insecticidal device balance adjustment method, and a program that enable adjusting of the position of an insecticidal device hanging from a robot. [Solution] In th...
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WO/2018/003082A1 |
[Problem] The purpose of the present invention is to provide a mobile body control application and a mobile body control method with which it is possible to spray a chemical agent efficiently. [Solution] The mobile body control applicati...
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WO/2018/003079A1 |
[Problem] To provide a drone accessory control system, a drone accessory control method, and a program that are able to restore an accessory suspended from a drone to a reference position 320 when the accessory has moved therefrom. [Solu...
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WO/2017/221859A1 |
[Problem] The present invention addresses the problem that functional components for causing multiple moving bodies to operate in a coordinated manner have to be designed individually in conformity to functional components for causing th...
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WO/2017/221560A1 |
[Solution] A flight control unit 201 causes one or a plurality of unmanned aerial vehicles 12 to fly along a flight path in a prescribed area. When a wireless device 11 of the unmanned aerial vehicle 12 detects a close-range wireless rad...
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WO/2017/221123A1 |
The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one...
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WO/2017/221122A1 |
The present disclosure provides methods and system for controlling the operation of a fly- by-wire aircraft. One or more yaw commands are received from an operator control, and one or more actual induced rolls rates are determined based ...
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WO/2017/216972A1 |
The present invention allows an unmanned aircraft to fly while avoiding a flight prohibited area, which changes depending upon the movement of a mobile unit. This unmanned aircraft control system (1) includes: a mobile unit position acqu...
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