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WO/2021/186179A1 |
A device having an input element, an output element, and a drive element, the device having a first position configured such that the drive element is engaged with the input element and the output element to prevent movement of the input...
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WO/2021/183453A1 |
This disclosure describes a ground station configured to facilitate the delivery of payloads using unmanned aerial vehicle (UAV). The ground station includes multiple sensors that allow for autonomous operation of the ground station as p...
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WO/2021/181717A1 |
Provided is a communication control apparatus for controlling an antenna of a flying object having the antenna for forming a cell in a target area on the ground by radiating a beam, and providing wireless communication services for user ...
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WO/2021/181554A1 |
An aircraft control device (20) that comprises a display unit (210), a display (220), an input unit (230), a selection unit (240), and a command generation unit (250). The command generation unit (250) acquires an image that has been gen...
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WO/2021/166677A1 |
A method for controlling an aircraft 1, the method comprising causing the aircraft 1, which is provided with a power storage device 7 and a power generation device 5 having a solar cell, to take off and/or rise by causing the power stora...
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WO/2021/165150A1 |
The hydraulic servo actuator contains a piston rod (3) and two pistons (K1, K2) which are arranged in tandem thereon and each of which is movably mounted in a separate hydraulic cylinder (Z1, Z2). Two separate redundant hydraulic circuit...
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WO/2021/153175A1 |
The objective of the present invention is to realize a configuration for receiving collision risk information from a mobile device such as a drone, generating a corrected path having low collision risk, and performing movement in accorda...
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WO/2021/149415A1 |
An electrohydraulic circuit (1) and an aircraft comprise: a supply oil path (90) connecting an oil supply device (10) that supplies hydraulic oil, and a drive unit (20) driven by the hydraulic pressure of the hydraulic oil supplied from ...
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WO/2021/149416A1 |
Provided are a selector valve, an electro-hydraulic circuit and an aircraft that are lightweight and capable of suppressing an overload. A selector valve 30, an electro-hydraulic circuit 1 and an aircraft comprise a sleeve 32, which is p...
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WO/2021/130061A1 |
Disclosed is an aircraft control system (100) comprising an input interface (102), an output interface (114) and a processing engine (108) comprising a classifier (110). The classifier (110) applies input data (104) generated by the inpu...
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WO/2021/133347A1 |
The present invention relates to a floor (z) located on air vehicles; a body (2) located on the floor (z); an arm (3) which extends on the body (2) in its entire length and located such that it is movable on the body (2); at least one sp...
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WO/2021/132696A1 |
A cover member according to the present invention is provided with: a transparent substrate having a first main surface and a second main surface; and a transparent first function layer that is laminated on the first main surface of the ...
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WO/2021/130032A1 |
Actuator for moving an aircraft control part, the actuator comprising: a mobile element movable in a first direction and in a second direction; an actuating means for moving the mobile element (2); a mechanical brake which, in case of lo...
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WO/2021/121941A1 |
The invention relates to an aircraft control column (M), the control column (M) comprising a first shaft (A1) and a control lever (1) configured to rotate the first shaft (A1) about a first axis (A) through a first angular range [α1; α...
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WO/2021/126018A1 |
Embodiments herein disclose e.g. a method performed by a mobile device (15) for handling identification of equipment. The mobile device records an image, in a recording direction at a first location, of the equipment. Upon recording the ...
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WO/2021/121939A1 |
The invention relates to a force application device (D) for an aircraft control column (M), the control column (M) comprising a control lever (l) configured to rotate a first shaft (A1) and a second shaft (B1), the force application devi...
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WO/2021/115167A1 |
A determination apparatus, comprising a circuit. The circuit is configured to: acquire first illuminance measured, in a first time period, by an illumination sensor (500) comprised in a flight body; acquire at least one first variation o...
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WO/2021/118925A1 |
A system for in-flight stabilization including a plurality of flight components mechanically coupled to an aircraft, wherein the plurality of flight components includes a first flight component and a second flight component opposing the ...
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WO/2021/112158A1 |
A flight control system (1) for an unmanned aerial vehicle comprising a total station (2) for tracking an unmanned aerial vehicle (3) having a reflector 7 mounted thereon and the reflector and acquiring measurement data including three-d...
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WO/2021/105303A1 |
The invention concerns an aircraft piloting system comprising a control system (4) configured to actuate flight controls (6) of the aircraft depending on a preprogrammed flight path, the control system comprising an autopilot system (8),...
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WO/2021/098917A1 |
The invention relates to an apparatus for controlling an actuating system of an aircraft in an open-loop and closed-loop manner. The apparatus has a first input interface, which is designed to receive first input data indicating a refere...
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WO/2021/097809A1 |
A method for an unmanned aerial vehicle (UAV) includes: generating a control signal that controls multiple motors of the UAV each configured to drive a corresponding one of multiple propellers. The multiple propellers are configured to b...
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WO/2021/094245A1 |
To extend the flight envelope (18) of an aircraft (1), which has a pair of wing halves (4) and extendable leading-edge flaps (11) at leading wing edges (10) of the wing halves (4), towards higher transonic flight Mach numbers, at least o...
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WO/2021/094712A1 |
According to an aspect of the invention, there is provided a weapon system for use on a vehicle, comprising: a control system, the control system configured to, in response to a determination that a line-of-sight from the weapon system t...
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WO/2021/095514A1 |
[Problem] To provide a turbulence sensing system and turbulence sensing method that make it possible to more safely and reliably suppress airframe shaking when turbulence is encountered. [Solution] This turbulence sensing system 10 compr...
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WO/2021/090352A1 |
A first attitude estimation unit 16 estimates an attitude of a UAV 1 by performing Visual-SLAM based on a detection value detected by an imaging unit 14, and a second attitude estimation unit 17 estimates the attitude of the UAV 1 based ...
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WO/2021/083822A1 |
An aircraft wing (2) having a main wing (3) and a trailing edge flight control surface (4) movable between a retracted position, a first extended position in which the control surface is positioned rearwardly in the chord wise direction ...
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WO/2021/087139A2 |
An airplane rudder and brake pedal assembly includes a rudder arm assembly having one rudder arm with first upper and lower arm portions, and another rudder arm with second upper and lower arm portions. The rudder arm assembly is assembl...
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WO/2021/079794A1 |
The present invention enables high-speed autonomous flight of a flying body. In the invention, a three-dimensional real-time observation result is generated on the basis of self-position estimation information and three-dimensional dis...
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WO/2021/080654A1 |
A gear drive, such as for an actuator, is a right-angle drive where toothed outer ridge of a face gear is coupled to teeth of a motor output shaft, and a set of planetary gears are engaged with a central sun gear of the face gear. The su...
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WO/2021/079075A1 |
The present invention relates to a force application device for a control stick of an aircraft comprising a shaft and a control lever configured to rotate the shaft about a first axis, the device comprising: a magnetic brake comprising a...
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WO/2021/079778A1 |
Proposed is a feature with which collision between an obstacle and a moving body can be avoided by performing an action to investigate an object difficult to be recognized. The moving body according to this feature has a control unit. Th...
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WO/2021/071390A1 |
The invention relates to the field of guided missiles, and more particularly to a mechanism for deploying folded aerodynamic control surfaces or wings of unmanned aerial vehicles. A mechanism for deploying an aerodynamic control surface ...
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WO/2021/069994A1 |
Described is a mechanical transmission (T) comprising a containment structure (1) housing a roto-translational element (2), extending along an axis of rotation (X) and comprising a first and a second threaded portion (3, 4), a rotary ele...
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WO/2021/070263A1 |
[Problem] To provide an aerial vehicle capable of achieving easy maneuverability during operation. [Solution] An aerial vehicle according to the present technology comprises: a vehicle body extending in the front-rear direction; a saddle...
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WO/2021/070464A1 |
A mobile body (200) comprises a generating unit (264), a first communication unit (220), a second communication unit (230), an obtaining unit (265), a providing unit (266), and an integrating unit (267). The generating unit (264) generat...
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WO/2021/069981A1 |
Described is a rotary mechanical transmission (T), comprising: a containment structure (1), a first rotary element (5), connected or connectable to a drive unit to define a mechanical power input unit and rotatable about an axis (X). The...
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WO/2021/070253A1 |
A flight system includes an aircraft that comprises a sensor and that can fly unmanned. The flight system estimates the state of dust in a planned destination area based on sensing data obtained by observing the planned destination area ...
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WO/2021/070518A1 |
According to the present invention, an aircraft is moved to a target landing point more accurately and quickly. This aircraft position control system comprises: a relative position acquisition unit which acquires the relative position be...
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WO/2021/065543A1 |
The present disclosure relates to an information processing device, an information processing method, and a program that enable more certain avoidance of collision with an obstacle. An avoidance orbit setting unit sets, on the basis of p...
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WO/2021/063842A1 |
The invention relates to a system for updating data for computing devices in an aircraft (10), the computing devices (1401) being likely, during the updating of the computing device data, to affect or not affect the safety of an operator...
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WO/2021/059787A1 |
A control device of this embodiment comprises: an acquisition unit that acquires information indicating the strain of a vane of a structure, and information indicating a control amount of a movable vane of the structure; a first determin...
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WO/2021/054178A1 |
The present disclosure relates to an unmanned aerial vehicle, a control method, and a program which make it possible to safely achieve interaction with an object to be recognized. A state estimation unit estimates the state of the object...
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WO/2021/051785A1 |
An electromagnetic steering engine and an aircraft. The electromagnetic steering engine comprises a driving coil (10), a permanent magnet (11), a coil fixing holder (12), and a permanent magnet fixing holder (13); the permanent magnet (1...
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WO/2021/053021A1 |
Disclosed is an aircraft system (10) for an aircraft (1). The aircraft system comprises a controller (100) that is configured to receive at least one signal during a take-off procedure of the aircraft. The signal may comprise information...
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WO/2021/053320A1 |
A method for assisting a pilot to navigate an aircraft when taxiing is disclosed. A centre line of a route, conformal to outside scenery, is displayed on an eyes out screen associated with the pilot. A pictorial indication of the alignme...
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WO/2021/052908A1 |
In order to improve space allocation, reduce weight and increase aerodynamic performance in high-lift devices (20), an actuator arrangement (24) for a fixed leading edge member (26) is proposed. The fixed leading edge member (26) has an ...
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WO/2021/053929A1 |
An aerial vehicle comprises a control unit that obtains tilt information about a tilt of a landing point and sets a horizontal speed according to the tilt information.
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WO/2021/045064A1 |
[Problem] To adapt to changes in conditions that can occur while a mobile terminal is mid-flight following a flight path and land the mobile terminal at a suitable landing position. [Solution] A control system 100 comprises: an informati...
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WO/2021/039245A1 |
This distribution device (10) is provided with an acquisition unit (11) which acquires position information about an obstacle, and a distribution unit (12) which wirelessly distributes, from the obstacle to an aircraft, obstacle informat...
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