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Matches 1 - 50 out of 3,365

Document Document Title
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...  
WO/2018/182944A1
An autonomous drone integrated with wide bandwidth, high energy acoustic wave generators sent to evict and eradicate agricultural pests within a patrolling area. The drone hovering close to a plant bombards its leaves and fruits with hig...  
WO/2018/173024A3
This invention is a security method for identifying possible attacks, suicide people or hijacking attempt, which allows identifying physiological behaviour patterns as for example: anxiety, nerves, stress and others, reading internal pat...  
WO/2018/161646A1
A propeller protection apparatus (130), an arm (120), and an unmanned aerial vehicle (100). The propeller protection apparatus (130) comprises a protective rod (132), a connecting rod (134), and a holding portion (136). One end of the co...  
WO/2018/164710A1
A boarding guidance system includes a beacon (202A) associated with a passenger seat (400A). The beacon is configured to communicate (506) with a passenger guiding device (102) and determine a distance between the passenger guiding devic...  
WO/2018/158258A1
Aircraft Ground Proximity Detection The present invention provides a system for detecting proximity of a ground service equipement (GSE) to a stationary aircraft comprising at least one GSE monitoring device adapted to be mounted to a GS...  
WO/2018/155534A1
The present invention makes it possible for a worker to readily reach a damaged point of an airframe and serves to reduce downtime of the airframe required for repairs. The present invention includes: a damage discriminating unit (21) th...  
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...  
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...  
WO/2018/155536A1
In order to accurately detect damage in an aircraft (1), using only a small number of sensors, the present invention comprises: a classification creation unit (11) that places aircraft having similar usage environment information into th...  
WO/2018/156335A3
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...  
WO/2018/149255A1
The present invention relates to intelligent warehousing technology. Provided in the present disclosure are a parachute system and a safety protection method for an unmanned aerial vehicle. The parachute system for an unmanned aerial veh...  
WO/2018/141470A1
The invention relates to a method for producing electric energy by means of a fuel cell system operated using a reformate gas, said method comprising the following steps: preparing a fuel cell system with a first reactor (R1) for convert...  
WO/2018/144576A1
A technique for adaptively disrupting UAVs detects a target UAV using a camera, monitors the target UAV's communications using a directional antenna aligned with the camera, and attempts to communicate with the target UAV to request that...  
WO/2018/140069A1
An ejectable flight data recorder for robust retention of flight data and aiding in locating an aircraft after an emergency situation comprises: a buoyant housing comprising an internal cavity, a door for access to at least a portion of ...  
WO/2018/133006A1
A landing gear control method and device for an unmanned aerial vehicle, user equipment unit, unmanned aerial vehicle, and unmanned aerial vehicle system. The method comprises: detecting whether a ground height of an unmanned aerial vehi...  
WO/2018/117878A1
The subject of the invention is a device protecting the flight data recorder ejected from an aircraft, whose task is to provide protection against physical damage of the flight data recorder during a plane crash and to assist reliable se...  
WO/2018/117627A1
An unmanned aerial vehicle (UAV) is provided. The UAV includes a first guard grill, a second guard grill configured to be removably combined with the first guard grill and form an external structure and an inner space of the UAV with the...  

Matches 1 - 50 out of 3,365