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Matches 1 - 50 out of 4,091

Document Document Title
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 ...  
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 ...  
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 ...  
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...  
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.  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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 ...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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 ...  
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...  
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...  

Matches 1 - 50 out of 4,091