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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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.
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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...
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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...
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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 ...
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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 ...
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WO/2018/111073A1 |
The present invention describes a system for controlling a focussed-signal antenna for extreme-distance drone tracking, achieving an effective communication range of 10 km with said aerial vehicle. The system includes an antenna with an ...
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WO/2018/109903A1 |
There is a need to reduce damage to objects due to contact with a rotating rotary wing. A flight control method controls the control mode during flight of an unmanned aircraft, the method having a step for detecting abnormalities in the ...
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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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