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WO/2017/217287A1 |
In the present invention, errors in longitude/latitude information in map data compared with actual longitude and latitude are eliminated, and an operator causes an unmanned aircraft to fly autonomously to a destination indicated in the ...
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WO/2017/208353A1 |
[Problem] To provide a drone automatic flight control application, a smart device, a drone, a server, a drone automatic flight control method, and a program, such that safety and convenience is enhanced. [Solution] A drone automatic flig...
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WO/2017/208354A1 |
[Problem] To provide a drone flight control system which makes it possible to improve the efficiency of pest control using a drone. [Solution] This drone flight control system 1 is provided with: a distance measurement module 101 for mea...
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WO/2017/208468A1 |
[Problem] To provide a drone flight control system which makes it possible to improve the efficiency of pest control using a drone. [Solution] This drone flight control system 1 is provided with: a distance measurement module 101 for mea...
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WO/2017/208355A1 |
[Problem] To provide an unmanned aircraft flight control application which detects a person at low cost with high performance, and performs control so that an unmanned aircraft does not crash with the detected person. [Solution] This unm...
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WO/2017/207666A2 |
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...
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WO/2017/208754A1 |
An information processing device 20 is provided, for example, to a vehicle 40. A control unit of the information processing device 20 provides flight control of an unmanned aerial vehicle 50, moves the same to a destination, and acquires...
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WO/2017/209974A1 |
A drone with a high-voltage trap seeks, identifies, pursues and destroys flying insects within a patrolling area. During its passive attracting mode, the drone lands on a designated ground site and attracts insects with light, sound, and...
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WO/2017/209796A1 |
Systems and methods for operating control surfaces of an aircraft. The method involves receiving, by an aircraft control system from one or more sensors, deflection information related to a shape and motion of an aircraft, and decomposin...
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WO/2017/203552A1 |
In order to provide an unmanned aircraft with which it is possible to minimize damage due to crashes caused by malfunction during flight, etc., a flight route is set on map information including a fall avoidance region, a control is perf...
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WO/2017/204050A1 |
The objective of the present invention is to make it possible for an inspection operator to carry out a hammering sound inspection without it being necessary for the inspection operator to perform an operation to move an inspection devic...
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WO/2017/201697A1 |
Techniques are disclosed for controlling a movable object based on gesture-based inputs. A client device (304) can receive image data associated with a first view from an image capture device (312). The client device (304) can detect a g...
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WO/2017/201267A1 |
Apparatus and method for actuating a double-slotted flap (26) movably coupled to an aircraft wing (12) are disclosed. An exemplary method comprises actuating a first panel (26A) of the double-slotted flap (26) relative to a structure of ...
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WO/2017/200441A1 |
The present invention regards a system and a method for providing a motion of an aircraft secondary control member (111, 611) incrementally in steps. An aircraft secondary control system comprises a rod arrangement (109, 609) of a drivin...
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WO/2017/191623A1 |
A system for real-time remote precision geo-pointing. The system includes at least two alignable aircraft, maneuver-able so as to create a line of sight (LOS) alignment with a target; a CPU/computer configured to calculate the position o...
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WO/2017/187300A1 |
Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronica...
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WO/2017/188041A1 |
Provided is a drop-release device capable of drop-releasing a payload on a target location from a small unmanned aircraft. This drop-release device comprises a small unmanned aircraft equipped with a plurality of rotor blades, a carrier ...
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WO/2017/185121A1 |
The invention relates to an aerodynamic profiled body (1) for an aircraft, in particular a winglet, comprising a front profiled element (2) having a profile front edge (4a), a rear profiled element (3) having a profile rear edge (3a), an...
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WO/2017/188587A1 |
An aerial vehicle having incline-controllable wings, according to one embodiment, can comprise: a body; a thrust part connected to the body and having a propeller and a rotary shaft; and the wings respectively arranged at both sides of t...
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WO/2017/185106A1 |
A system for RF communications with UAVs which includes two distinct frequency bands, one for optional use to support datagrams between a UAV payload and a computer or controller and a second RF communications band dedicated to command a...
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WO/2017/184437A1 |
An unmanned aircraft includes a forward propulsion system comprising one or more forward thrust engines and one or more corresponding rotors coupled to the forward thrust engines; a vertical propulsion system comprising one or more verti...
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WO/2017/182835A1 |
There is provided a control stick module (10) comprising: a first shaft (100); a second shaft (110); a joint (140) connecting the first and second shafts; and a gimbal mechanism (120); wherein the joint is nested within the gimbal mechan...
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WO/2017/182836A1 |
A control stick pivot (200) comprises a primary pivot bearing (210), a redundant pivot bearing (220), and a detection component for detecting malfunction of the primary pivot bearing. The redundant pivot bearing is provided on one side o...
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WO/2017/178790A1 |
An aircraft (101) is provided with a single centrally located inceptor (110) for controlling pitch and roll of the aircraft. The inceptor (110) is provided with a double grip (11, 112) so that it may be comfortably operated by either a p...
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WO/2017/180392A1 |
The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module op...
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WO/2017/175804A1 |
[Problem] To provide a method for controlling the flight of a drone that performs accurate chemical spraying on agricultural land having a narrow and complex topography. [Solution] At least one reference point pole is installed at a boun...
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WO/2017/169841A1 |
The objective of the present invention is to improve the convenience of a display device or a display control method for displaying captured images from a moving body, such as making it possible for an operator to see the moving body wit...
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WO/2017/170651A1 |
A work management system (SYS) according to an exemplary embodiment of the present invention comprises a shovel (100), an aircraft (200) provided with a camera (205), and a management device (300), and is provided with: a progress region...
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WO/2017/170148A1 |
Provided is a flight device that comprises: a flight unit; and a flight control unit which performs, in a case where the flight position of the flight unit is outside a prescribed range, control different from control performed in the ca...
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WO/2017/169516A1 |
An image projection unit 101 projects an image containing identification information for identifying control content for an unmanned flying device onto an object to be inspected. A control unit 103 controls the operation of the unmanned ...
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WO/2017/173159A1 |
Unmanned Aerial Vehicles also known as UAVs or Drones, either autonomous or remotely piloted, are classified as drones by the US Federal Aviation Administration (FAA) as weighing under 212 pounds. The system described herein details Auto...
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WO/2017/172840A1 |
This document describes a system and method through which unmanned aerial vehicles (UAVs) can be docked, with a device that can secure the UAVs, and information can be transmitted to and from such UAVs. The UAVs are secured through the u...
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WO/2017/168457A1 |
[Problem] To provide an automatic tracking image pickup system that accurately measures, using three-point measurement, and compares and calculates positional information of a moving image pickup body, such as a flying object on which an...
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WO/2017/163587A1 |
A vertical takeoff and landing aircraft 1 according to an embodiment of the present invention includes: a pair of ducted fans 2; a body 3 which is disposed below the ducted fans 2; a frame body 4 which connects the body 3 and the ducted ...
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WO/2017/165481A1 |
An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provi...
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WO/2017/154421A1 |
This flying object (10) comprises: a plurality of rotor units (30) each including a propeller (32) and a motor (33) that drives the propeller (32), the plurality of rotor units producing thrust for causing the flying object (10) to fly; ...
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WO/2017/154474A1 |
This flying object (10) comprises: a plurality of rotor units (30) each including a propeller (32) and a motor (33) that drives the propeller (32); a balloon (20) that covers the lateral sides of the plurality of rotor units (30) so as t...
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WO/2017/154551A1 |
This flying object (100) comprises: a plurality of rotor units (20) each including a propeller (21) and a motor (22) that drives the propeller (21); a plurality of balloons (30) respectively provided to the plurality of rotor units (20);...
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WO/2017/149541A1 |
A flap actuator for adjusting the orientation of a flap or the like, the actuator. The actuator includes: a static arcuate member having a radius of curvature; a piezoelectric motor biased to be in operable contact with the static arcuat...
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WO/2017/150433A1 |
Provided is a technique whereby operability and working efficiency of flight control for an unmanned air vehicle can be improved. A photographing unit 81 photographs a projection object onto which light is projected after being outputted...
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WO/2017/151082A1 |
The utility model relates to the sphere of aviation and aircraft repair technology, namely to the Method of on-condition repair and modernization up-dating of an aircraft hydraulic system, in particular, of Antonov-32 (An-32) type aircra...
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WO/2017/151493A1 |
A redundant control system (10) for a vehicle includes: one or more actuator housings (202); a plurality of actuator pistons (212a, 212b) coupled to the actuator housings, each of the actuator pistons mechanically coupled to one another ...
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WO/2017/148591A1 |
The present invention relates to a high-lift system of an aircraft comprising flaps arranged on the wings of the aircraft, and also comprising a central drive and drive shafts, of which in each case one extends into one of the wings star...
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WO/2017/151081A1 |
The utility model relates to the sphere of aviation and aircraft repair technology, namely to the Method of on-condition repair and modernization up-dating of an aircraft center wing section, in particular, of Antonov-32 (An-32) type air...
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WO/2017/144176A1 |
The invention relates to an aircraft comprising at least one component and at least one electronic device for controlling the component, wherein the electronic device has at least one interface, by means of which signals can be provided ...
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WO/2017/138049A1 |
The control system (100) includes a flying body (10) and a base station (50). The base station is equipped with a light source unit which irradiates guide light of a predetermined wavelength. The flying body is equipped with: a propulsio...
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WO/2017/137918A1 |
Servo actuator comprising: a shaft, an engine; a first member (4) dragged by the engine (3); a second member (5) coupled slidingly to the shaft (2) in order to be engaged in/disengaged from the first member (4); first spring means (6); a...
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WO/2017/131834A2 |
A pivoting wing system, capable of vertical take-off and landing, having a hub connected to one or more wings provided on a spanwise axis. The wings are further provided with one or more thrust producing devices mounted to the top and bo...
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WO/2017/131823A2 |
An unmanned aerial combat vehicle system is disclosed. The system provides for an unmanned aerial combat vehicle that is capable of performing reconnaissance, disrupting enemy communications, or delivering a weaponized payload. The unman...
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WO/2017/123987A1 |
An actuator assembly comprising an output member rotatable about an output axis, first and second actuators each having an axis of rotation, a drive motor and a hold motor, first and second linkages between each of the first and second a...
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