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WO/2024/059347A1 |
A system having components coupled to an aircraft that measure the navigational state and state uncertainty of an aircraft. To do so, the aircraft captures an image of its surrounding environment including an object of interest and appli...
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WO/2024/042309A1 |
Air data estimation involves determining values of air data parameters such as airspeed, altitude, angle of attack and angle of sideslip. Accurate determination of air data parameter values is crucial to enable accurate control of an air...
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WO/2024/037831A1 |
The invention relates to an air data indicating and calibrating arrangement (1) and method for a vertical take-off and landing aircraft, in particular a helicopter (50), for providing information on an air speed of the vertical take-off ...
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WO/2024/038249A1 |
A flow body unit (600) for a fluid flow rig (10) for simulating fluid flow patterns; the flow body unit (600) comprising: a flow body support frame (700); a core member (800) extending from the flow body support frame (700) along a flow ...
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WO/2024/032113A1 |
Provided in the present invention are a self-driving early-warning unit and early-warning method for stall of a moving body. The early-warning unit comprises: a triboelectric sensing unit, which comprises a friction electrode layer and a...
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WO/2023/207695A1 |
An optical display (303), a seat and a vehicle (1000). The optical display (303) comprises: a display main body (32), comprising a light-exit portion (11), a back portion (13) and a connecting side portion (15), the light-exit portion (1...
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WO/2023/196755A1 |
A display system is provided for a vehicle having a windshield (500) and vehicle structure (506) outside the windshield. The vehicle structure (506) is visible within a field of view defined by the windshield (500). Certain embodiments o...
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WO/2023/175784A1 |
A measuring system (1) comprises an aircraft (30) that flies in a measurement zone and performs measurement and a management device (10) that controls the flight path of the aircraft (30). The management device (10) comprises an informat...
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WO/2023/174678A1 |
The present invention provides a visual aid (200) for improving a pilot's awareness of the situation and status of an aircraft, which comprises means for: (202) determining, on the basis of information relating to the current navigation ...
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WO/2023/120908A1 |
The present invention provides a system for obtaining positional coordinates of a camera video object by using a drone having an onboard flight control computer, the system comprising: a global positioning system (GPS) configured to use ...
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WO/2023/119298A1 |
An unmanned aerial vehicle (UAV) is disclosed. The UAV comprises a body; a propulsion unit; a controller; and at least one adjustable camera unit. In some embodiments, each adjustable camera unit comprises, a camera; and a gimbal, mounti...
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WO/2023/114402A1 |
Systems, methods and computer-readable media for telemetry data visualization are described herein. The described system includes paths and reduced components in between reception of sensor data and display to an engineer, reducing time ...
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WO/2023/100133A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated ...
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WO/2023/100150A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described; the control unit (46, 46') is programmed to: - receive in input a plurality of data associated w...
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WO/2023/091481A1 |
A satellite having a longitudinally elongated body and being capable of operating in the thermosphere. The satellite can be powered by an electric rocket engine, and includes a remote sensing system configured to obtain images of Earth. ...
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WO/2023/075731A1 |
The present invention relates to a body (2) located at an air vehicle; a first structural part (3) located in the body (2) and carrying the loads on the body (2); a second structural part (4) located opposite the first structural part (3...
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WO/2023/055324A1 |
The present invention provides a body (2) provided at the air vehicle; at least one indicator (3) located on the body (2) and in the pilot's field of vision; at least one guide (4) located on the body (2) between the indicator (3) and th...
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WO/2023/047370A1 |
Aircraft (1) comprising: a moving system (10) adapted for use when the aircraft (1) is in flight to move sensing means (18) of the aircraft between a rest position, wherein the sensing means (18) are arranged within the aircraft, and a w...
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WO/2023/046280A1 |
The invention relates to an assistance apparatus (14) for an aircraft (10), said apparatus comprising: an electronic computing device (16) which has a memory (18) in which items of data are stored that characterise a plurality of flight ...
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WO/2023/044535A1 |
An emergency interface system for an autopilot system has an actuator mechanically interfacing an actuator switch, the actuator throwing the actuator switch when operated. The actuator switch has an actuator output connected to an input ...
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WO/2023/043604A1 |
An aircraft panel apparatus, assembly of aircraft panel and parts in and/or of an aircraft, and method of manufacturing the aircraft panel apparatus and parts is provided. These aircraft panel and parts can be used for a variety of singl...
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WO/2023/003336A1 |
A drone integrated control apparatus for controlling a drone, in which each component of the control apparatus is integrated on a single board, is characterized by comprising: a flight control unit which has a plurality of sensors and co...
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WO/2022/258534A1 |
The invention relates to a probe for measuring static or parietal pressure, comprising a pressure sensor module (1), a mounting plate (2) provided with air inlets (3) and intended to be mounted on the skin of an aircraft, and a shut-off ...
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WO/2022/258535A1 |
The invention relates to a pressure measurement probe for aircraft, comprising a pressure sensor board (1) that comprises an electronic board (2) equipped with a pressure sensor (3) provided with an air inlet (4), the electronic board (2...
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WO/2022/216511A1 |
The present application is directed to a video-based motion extraction system that uses mmWave imaging. In one example, an object velocity is extracted in real time from at least one motion vector obtained from a compressed video. The ve...
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WO/2022/194961A1 |
This aeronautical probe is characterized in that it has a profiled overall shape, which is provided with a fastening base (2) and at least part of the leading edge (5) of which comprises corrugations (6).
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WO/2022/133676A1 |
A method for detecting the arm state of an unmanned aerial vehicle, a control device, an unmanned aerial vehicle, and a storage medium. Two arms (10) of an unmanned aerial vehicle (200) are provided with a first positioning sensor (20) a...
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WO/2022/136981A1 |
It is disclosed an indicator (16a) for an aircraft (1) capable of hovering, comprising a first indication (35) associated to the value of vertical speed of the aircraft (1) itself; the indicator (16a) comprises a first area (100) wherein...
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WO/2022/120483A1 |
Disclosed herein is a detachable modular console for an aircraft cockpit. The detachable modular console comprises a housing configured to receive one or more modular electronic components, a plurality of hardpoint fasteners for detachab...
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WO/2022/101129A1 |
The invention relates to a method for determining at least one minimum power margin of a hybrid drive train for a transport vehicle, each drive element being associated with at least one power source and at least one power consumer, the ...
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WO/2022/094875A1 |
Provided are a positioning device (100), a remote control terminal, an unmanned aerial vehicle, and an unmanned aerial device. The positioning device (100) comprises a housing (10) and an RTK module (20), the housing (10) being provided ...
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WO/2022/038383A1 |
Disclosed is a pilot aircraft system control input arrangement for a light aircraft having primary flight controls, the pilot aircraft system control input arrangement integrated into an armrest for a pilot's seat, the armrest providing ...
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WO/2022/019257A1 |
Provided are a detection system, a suspended device, and a detection method capable of detecting a situation below the water surface under various environments. A flying body 1, including an unmanned flying body, such as a drone, and a...
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WO/2022/005420A1 |
The present invention relates to at least one screen (2) which is provided in air and/or space vehicles and displays graphic and/or video images created with flight data of the air and/or space vehicles; at least one data source (3) cont...
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WO/2021/255186A1 |
The invention relates, in particular, to an aircraft for flight training, the aircraft comprising, in particular, a fuselage (1) which extends along a longitudinal axis (D) of the aircraft, the fuselage (1) comprising a front end forming...
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WO/2021/228923A1 |
Disclosed is a method for guiding the pilot of an aircraft for the alignment manoeuvre, comprising: determining, at a first instant, an occurrence close to the alignment manoeuvre and triggering the display of a first symbol (30) on the ...
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WO/2021/224309A1 |
The present invention relates to a system for interacting with a plurality of visual zones comprising: - a measurement module (32) capable of generating a set of measurements characterising each position and/or orientation of at least on...
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WO/2021/173816A1 |
An angle of attack sensor includes a housing and a faceplate. A vane assembly extends through a central opening of the faceplate and includes a vane. The vane comprises a root, a tip, a leading edge, a trailing edge, a first lateral face...
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WO/2021/140491A1 |
A computer implemented method for estimating angles of attack (α) and / or sideslip (β) of a flying body comprises the steps of: Providing data or measurements representative of the time derivative of the module of a speed of the flyin...
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WO/2021/140554A1 |
[Problem] To provide an aircraft or the like for which the attitude can be more precisely ascertained. [Solution] The aircraft according to this invention comprises an airframe provided with a rotary wing unit; a plurality of sensors whi...
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WO/2021/134584A1 |
Disclosed are a motion sensor module and a movable platform. The motion sensor module comprises: a motion sensor (10); a bearing frame (20), used for bearing the motion sensor (10); a mounting frame (30), used for connecting an external ...
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WO/2021/116694A1 |
A pressure altering surface for use in an airspeed measurement system of an aircraft, the pressure altering surface comprising a fluid engaging exterior surface, the fluid engaging outer surface having a portion that is substantially dom...
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WO/2021/097439A1 |
In some embodiments, the present disclosure provides systems and methods enabling unmanned vehicle navigation and delivery including an integrated roofing accessory integrated into a roof, the integrated roofing accessory including at le...
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WO/2021/079360A1 |
A cockpit for an airplane having, in a plan view, an aft direction, a central longitudinal axis parallel to the aft direction and a rear axis perpendicular to the central longitudinal axis. The cockpit as seen in the plan view comprises:...
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WO/2021/062097A1 |
An aircraft airflow sensor including a vane assembly configured to sense a direction of local airflow outside an aircraft, at least one port arranged on the vane assembly, and at least one transducer arranged with the vane assembly confi...
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WO/2021/058819A1 |
The present invention relates to an optomechanical system (200) based on one or more optomechanical elementary cells (400), to the use of the optomechanical system to locally determine flow variables or accelerations, to a flow sensor as...
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WO/2021/042030A1 |
An aircraft airflow sensor probe configured to correct measurements based on aircraft movement includes a vane assembly configured to sense a direction of local airflow outside an aircraft, at least one accelerometer configured to detect...
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WO/2020/251647A1 |
A low visibility aid device includes a main body having a front end, a back end, a middle section and an interior space. A mounting bracket extends outward from the main body for securing the device onto a manned aircraft for use during ...
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WO/2020/247641A1 |
Systems and methods are directed toward determining a vehicle orientation based on sensor information. Sensors are positioned along a vehicle body that may be evaluated to determine corresponding values between matching sensor types. Whe...
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WO/2020/245588A1 |
There is disclosed an aircraft configured to collect air data, the aircraft comprising: a wing structure; a forebody, forward of the wing structure; an afterbody, backward of the forebody; a skin covering the wing, the forebody and the a...
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