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Matches 1 - 50 out of 3,418

Document Document Title
WO/2019/090755A1
Disclosed are a motion sensor assembly (10) and an unmanned aerial vehicle (100). The motion sensor assembly (10) comprises: a mounting support (1), a sensor assembly body (2), and a damping mechanism (3) connected between the mounting s...  
WO/2019/093198A1
The present invention avoids a collision with a flying body operated by another party, on the basis of the classification of said flying body. A detection unit detects the presence of another flying body (10A) within a prescribed range f...  
WO/2019/092914A1
This flying object safety device (90) is provided with a deployable body (86) and an ejection device (88). The ejection device (88) has: a container (80) that accommodates the deployable body (86) and has an opening provided at one end; ...  
WO/2019/090277A1
Embodiments of the present invention enable a user of a drone to operate it more quietly. Embodiments of the present invention relate to such a system, apparatus, and a method of and for a drone that may be quiet, that can fly far while ...  
WO/2019/089966A1
A technique for finding and estimating the locations of atmospheric thermals for the purpose of exploiting the updraft energy to enable the aircraft to remain aloft while reducing or eliminating the need to expend fuel or energy and oper...  
WO/2019/089597A1
Various aircraft systems may benefit from enhancements that increase the reliability of the systems. For example, certain avionics systems may benefit from a distributed aircraft recorder system. A system can include an aircraft recorder...  
WO/2019/081924A1
Diverse types of crew interfaces (400, 430, 450) are provided for outputting visible, audio and tactile information to a pilot for flight control. A unified estimation of the current aircraft state and of a current phase of flight are ma...  
WO/2019/084279A1
Various systems may benefit from appropriate triggers to action. For example, various deployable safety devices, such as emergency locator transmitters and flight recorders, may benefit from a multiple input release mechanism. A method i...  
WO/2019/080184A1
A device for protecting a camera of an unmanned aerial vehicle, comprising: a housing (1), the housing (1) comprising a first side surface (11) and a second side surface (12), the first side surface (11) being provided with a photographi...  
WO/2019/077963A1
The present invention comprises: a fuselage frame (10); a thrust unit (20) for generating thrust for flying; an airflow sensor (30) for acquiring airflow information relating to the surrounding airflow; and a control device (40) for cont...  
WO/2019/077457A1
An aircraft (100) is provided that includes a fuel storage tank (108) for aviation fuel, and avionics systems interconnected by an avionics bus. The fuel storage tank (108) receives aviation fuel during a fuel uplift for a flight accordi...  
WO/2019/071344A1
Apparatus and methods for assisting a flight crew with (e.g., pre-flight) functional testing of aircraft systems are disclosed. An aircraft condition can be used to select one or more functional tests that are applicable based on the air...  
WO/2019/069501A1
Provided are an aircraft soundness diagnostic device and an aircraft soundness diagnostic method that enable diagnosis of detachment and the progress or the like of detachment of an adhered structure in the body of an aircraft. An aircra...  
WO/2019/064981A1
Provided is an aircraft sensor module 21 disposed on an aircraft, said module comprising: energy harvesting elements 25 for generating energy by the internal and external environments of the aircraft; an electricity accumulation device 2...  
WO/2019/067083A1
An unmanned aerial vehicle comprising one or more sensors, configured to receive data from an area surrounding the unmanned aerial vehicle; one or more processors, configured to detect movement in a region surrounding the unmanned aerial...  
WO/2019/061386A1
An unmanned aerial vehicle fall protection device, comprising a vehicle body (1), the vehicle body (1) being fixedly connected to bases (3) by means of connecting rods (5), and inner portions of the bases (3) being provided with shock ab...  
WO/2019/056181A1
A method and device for positioning an unmanned aerial vehicle, as well as an electric adjustment and power system, and an unmanned aerial vehicle system, the method for positioning an unmanned aerial vehicle comprising: when detecting t...  
WO/2019/055722A1
One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the a...  
WO/2019/055140A1
Various embodiments include methods for rotor anomaly detection and response for an aerial robotic vehicle (100). A processor (220) of the aerial robotic vehicle may obtain data from a sensor (236, 237, 238) onboard the aerial robotic ve...  
WO/2019/054027A1
An acquiring unit of the present invention acquires a flight plan containing first flight conditions. A setting unit sets a risk level for airspace in which an aircraft is flying. A determining unit determines second flight conditions. A...  
WO/2019/054997A1
A computer-implemented method and system for controlling an aircraft based on detecting and mitigating fatiguing conditions and aircraft damage conditions is disclosed. According to one example, a computer-implemented method includes det...  
WO/2019/054236A1
Provided is a technology that can implement a status assessment of an aircraft in terms of identifying signs of anomaly before the occurrence thereof and assist a pilot in preparing for the anomaly. In the aircraft operations system 1, a...  
WO/2019/056009A1
A pitot tube cover (10,120) for a pitot tube (100) operable to determine a speed of an aircraft based on an airstream impinging on the pitot tube (100). The pitot tube cover (10,120) has a body (12,122) and a sail (14) extending from the...  
WO/2019/047073A1
An aerial vehicle landing method, an aerial vehicle, and a computer readable storage medium. The aerial vehicle landing method comprises: an aerial vehicle determining a dynamic target, the dynamic target being a target in motion; the ae...  
WO/2019/044125A1
This flying body comprises: a fuselage; a canopy capable of adjusting the speed of a fall when falling; a brake cord having one end connected to the canopy; a winding device (20) which is provided on the fuselage and allows the other end...  
WO/2019/041069A1
A flying robot, comprising a flying robot body and a damping device body (9). Both left and right sides of the damping device body (9) are equipped with a chest fixing plate (1) and a back fixing plate (4), and an arm fixing column (2) i...  
WO/2019/045242A1
The purpose of the present invention is to provide an unmanned aircraft black box system, which encrypts and stores flight data of an unmanned aircraft, transmits/receives the same to/from a ground control system and backs up the same in...  
WO/2019/039945A1
An aircraft monitoring device for providing tracking information as to the position of an aircraft during flight and a system including an aircraft-based monitoring device and a remote monitoring system. The aircraft monitoring system ma...  
WO/2019/036361A1
Methods and system are disclosed for guiding an autonomous drone aircraft during descent to a landing target. The method features the steps of: (a) acquiring an image using a camera on the drone aircraft of an active fiducial system at t...  
WO/2019/030820A1
In order to more reliably land a flying vehicle at a desired location, the flying vehicle is provided with: a determination means which determines whether the flying vehicle is taking off and ascending from a take-off point, or is descen...  
WO/2019/027171A1
The present invention relates to an unmanned drone for aerial survey, which makes an aerial flight by generating a lift force with rotation forces of propellers (11), the drone comprising: a drone body (10) including a battery and a remo...  
WO/2019/023322A1
A method, preferably including: sampling inputs, determining aircraft conditions, and/or acting based on the aircraft conditions. A method, preferably including: sampling inputs, determining input reliability, determining guidance, and/o...  
WO/2019/020630A1
The invention relates to a signal generator for unmanned aircraft, comprising at least one light source and/or at least one sound source and also at least one closed-loop/open-loop controller for operating the at least one source.  
WO/2019/023106A1
A combination of a visual warning cue and a conspicuous auditory warning cue acts synergistically to reduce bird strike frequency against a man-made structure. Methods and systems are described for providing said combination of warning c...  
WO/2019/018754A1
A broad good, comprising a plurality of fibers looped randomly throughout the broad good, a binder material binding the plurality of fibers together, the plurality of bound fibers forming a dimensionally stable nonwoven veil, a first met...  
WO/2019/011019A1
An aircraft control method, comprising: acquiring environmental brightness data by a brightness sensing device of an aircraft (S110); determining whether the environmental brightness data satisfies a brightness value required for normal ...  
WO/2019/013151A1
The present invention addresses the problem of providing a method for setting a flight altitude, and an unmanned aerial vehicle system, with which a flight altitude in a flight plan can be set efficiently in accordance with undulations a...  
WO/2019/003405A1
Provided is a landing apparatus which guides an unmanned aircraft to avoid obstacles and the like and lands the unmanned aircraft at a low-risk spot. The landing apparatus has a dangerous object position detecting device, a movement targ...  
WO/2018/234523A1
The invention relates to a method for detecting damage to a rotor of an aircraft, wherein the aircraft has actuators for actively reducing vibration, the method comprising the steps: determining actuator manipulated variables in a refere...  
WO/2018/230552A1
An assist system (10A) comprises: a detection unit (12) mounted in an aircraft capable of hovering, the detection unit (12) being provided on the outside of the fuselage (31), and detecting objects that could be obstacles; imaging units ...  
WO/2018/232196A1
The present disclosure relates to aircraft and aircraft flight control systems, methods, and apparatuses. A condition-aware aircraft configured to make in-flight decisions autonomously, based on the most up-to-date information, to perfor...  
WO/2018/223378A1
An unmanned aerial vehicle control method and device, and an unmanned aerial vehicle. The method comprises: acquiring state information about an unmanned aerial vehicle (S101); determining a control instruction according to the state inf...  
WO/2018/217210A1
A method for providing adaptive control to a fly-by-wire aircraft includes measuring via at least one first sensor a characteristic of at least one component of the aircraft and measuring via at least one second sensor a state of the air...  
WO/2018/196494A1
An unmanned aerial vehicle control method and device and an unmanned aerial vehicle, belonging to the technical field of unmanned aerial vehicle control. The method comprises: monitoring the running state of each power motor in an unmann...  
WO/2018/195214A1
An autonomous distress tracking system for an aircraft is described. The system can include a transponder configured to transmit radio frequency (RF) emissions and an RF detector unit configured to detect the RF emissions. The system can...  
WO/2018/189299A1
An uplock (101) for use with an aircraft component. The uplock comprises a hook (102) configured to engage a capture pin (126) mounted on the aircraft component. The hook (102) is mounted for movement between a closed position and an ope...  
WO/2018/189249A1
The invention relates to a device (1) for measuring rotor blade movements of an aircraft over the entire rotor rotation in flight, having at least one rotatably arranged rotor blade (2) and an image recording unit (4) for recording image...  
WO/2018/187701A1
Some embodiments described herein relate to a drone landing platform. One or more sensors (122A) coupled to the drone landing platform (120A) can detect local conditions in the vicinity of the drone landing platform. A communications sys...  
WO/2018/183871A1
A carpet tile having a greige good, an adhesive layer, and a secondary backing material. The greige good has a primary backing component and a plurality of fibers attached to the primary backing component. The adhesive layer has an adhes...  
WO/2018/182797A1
This document describes a system and method through which unmanned aerial vehicles (UAVs) and other vehicles (e.g., unmanned underwater vehicles (UUVs), also known as autonomous underwater vehicles (AUVs), unmanned water-surface vehicles...  

Matches 1 - 50 out of 3,418