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Matches 1 - 50 out of 658

Document Document Title
WO/2019/124686A1
A flight controller of a vertical take-off and landing aircraft, according to one embodiment of the present invention, controls a tilt angle of a main rotor on the basis of a vertical posture control signal in a low-speed flight state. W...  
WO/2019/099538A1
Systems and aircraft are provided. An avionics system includes a storage device and one or more data processors. The storage device stores instructions for monitoring an actual performance of the aircraft. The one or more data processors...  
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/2019/082063A1
The present invention relates to a control device with control panel (1) for air vehicles and for controlling the suitability of inputs entered into the control panel (CP) by a pilot in order to operate air vehicle and to give automatic ...  
WO/2019/061000A1
The present disclosure provides methods and systems for providing a lateral center of gravity of an aircraft on an aircraft display. A fuel distribution in the aircraft fuel tanks is determined. A lateral center of gravity of the aircraf...  
WO/2019/059889A1
A portable computerized device for an aircraft control system includes an input system for inputting commands, a device display for displaying information on the computerized device, a processor, a wireless communication module, and a no...  
WO/2019/053058A1
The invention relates to an autogyro (1), comprising a rotor (3), which can be set into autorotation, an instrument panel (9), which has at least one display unit (11) and/or at least one operating unit (12), the instrument panel (9) hav...  
WO/2019/043645A1
A method and a system are disclosed for determining an estimation of an anemometric parameter of an aircraft, the anemometric parameter selected from a group comprising at least one of an angle of attack, a sideslip angle and a calibrate...  
WO/2019/016930A1
The present invention determines, with a high degree of accuracy, the magnitude of influence exerted by wind on a moving body from information acquired from the moving body. This data processing device is provided with: an acceleration a...  
WO/2019/018805A1
A method of calculating a climb-dive marker (CDM) that is visibly present on a display even as the aircraft approaches a roll angle of +/- 90° is provided. An exemplary CDM method comprises obtaining, an X-axis velocity, a Y-axis veloci...  
WO/2019/000397A1
Provided in the present invention is an unmanned aerial vehicle (100), comprising: a fuselage (10), a rotor assembly and a barometer (40); the rotor assembly is disposed on the fuselage (100), and the barometer (40) is disposed outside o...  
WO/2018/236181A1
The present invention relates to a mobile platform-based AHRS flight control apparatus and, more specifically, to a mobile platform-based AHRS flight control apparatus of an unmanned flying object comprising a drone frame (10) on which a...  
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/2018/209770A1
A barometer assembly (10) and a drone (100). The barometer assembly (10) is used in the drone (100). The drone (100) comprises a central frame (20), an arm (30) extending outwards from the central frame (20), a power assembly (40) dispos...  
WO/2018/167472A1
The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization unit...  
WO/2018/102318A1
In accordance with at least one aspect of this disclosure, a computer implemented method includes receiving imaging data from an imaging system of an aircraft, and creating a new flight plan or a modified flight plan of the aircraft base...  
WO/2018/094824A1
A fixing buckle (50) and an unmanned aerial vehicle (100) having same. The fixing buckle (50) is used for fixing a sensor (70) on a support, and comprises a buckle body (51) and a limiting part (511) provided on the surface of the buckle...  
WO/2018/081559A1
An air data probe (10) and associated method of method of measuring air data is disclosed. The air data probe includes a plurality of air pressure sensors, and a body (14) that encloses a hollow interior cavity (16), where the body (14) ...  
WO/2018/070103A1
Provided are a detachable unit that makes it possible to make work for calibrating the various sensors provided to an unmanned aerial vehicle more efficient and to unitize an unmanned aerial vehicle control function, and a sensor calibra...  
WO/2018/060392A1
Aircraft comprising a fuselage (1) divided by a floor (2) into an o upper volume (3) and a lower volume (4) through which joists (5) extend that support the floor and delimit, along with the fuselage and the floor, two side chambers (6),...  
WO/2018/043988A1
Disclosed are an unmanned aerial vehicle for aerial reconnaissance, which performs object detection and object hitting on the basis of image information, and an unmanned defense system and method using the same. The unmanned aerial vehic...  
WO/2018/011791A3
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...  
WO/2018/002878A1
An aircraft avionic system for use in an equipped aircraft includes a controller and a display. The controller provides output data to the display, with the output data producing visual images on the display. An angle of attack data sour...  
WO/2017/221859A1
[Problem] The present invention addresses the problem that functional components for causing multiple moving bodies to operate in a coordinated manner have to be designed individually in conformity to functional components for causing th...  
WO/2017/208179A1
The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-...  
WO/2017/191543A1
Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the ...  
WO/2017/162862A1
The invention concerns an aircraft probe for resisting formation and propagation of ice comprising: • a base that is intended to be attached to an aircraft; • a housing extending from the base, said housing comprising:  a body ext...  
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...  
WO/2017/073241A1
Provided is a technique with which it is possible to measure the airspeed of a low-speed flight vehicle along a horizontal direction. An airspeed measurement system for a low-speed flight vehicle, wherein the airspeed measurement system ...  
WO/2017/055975A1
A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative...  
WO/2017/053913A1
A truss-reinforced radome crown structure (TRRCS) that functions in combination with an aircraft and a communication radome or antenna. The TRRCS maintains and protects a radome and antenna located on an aircraft's fuselage. The TRRCS in...  
WO/2017/021414A1
A display management system 10 is provided for displaying a graphical representation of flight envelope information of an aircraft. Included in the display management system is a control module 20 being coupled to the display management ...  
WO/2017/002055A2  
WO/2016/209225A1
Examples disclosed herein relate to control of a drone. In one example, aerial movement of the drone is controlled. In the example, it is determined, based on a plurality of devices, whether the drone is within a line- of-sight with at l...  
WO/2016/204843A3
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain...  
WO/2016/204843A2
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain...  
WO/2016/195816A2
An avionics display for rotorcraft provides a depiction of 360 degrees of terrain and obstacles about the rotorcraft using a top plan view at above a predetermined altitude that transitions to an angle perspective view as the altitude dr...  
WO/2016/195816A3
An avionics display for rotorcraft provides a depiction of 360 degrees of terrain and obstacles about the rotorcraft using a top plan view at above a predetermined altitude that transitions to an angle perspective view as the altitude dr...  
WO/2016/190933A3
Vehicle navigation methods, systems and computer program products are provided that create a composite video image of a scene from video images of the scene generated by a plurality of video image sensors. The video image from each image...  
WO/2016/190933A2
Vehicle navigation methods, systems and computer program products are provided that create a composite video image of a scene from video images of the scene generated by a plurality of video image sensors. The video image from each image...  
WO/2016/164624A1
A system for and method of indicating an angle of attack of an aircraft is provided. The system utilizes measurements from existing aircraft sensors so that a dedicated angle of attack sensor is not required. The system enables and benef...  
WO/2016/130716A2
A method of unmanned aerial vehicle (UAV) operation, including: receiving from a customer a first data request (400), the first data request (400) having: a first geographic coverage area, and a refresh rate for the first geographic cove...  
WO/2016/130721A2
A method of migrating unmanned aerial vehicle (UAV) operations between geographic survey areas, including: uploading a first plurality of flight missions (604) into a first UAV pod; deploying the UAV pod (606); autonomously launching the...  
WO/2016/125139A2
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...  
WO/2016/105324A1
The group of inventions relates to means for enhancing vehicle safety. An autonomous modular device contains means for recording, controlling and reacting, signaling means, an electronic module, a cluster module, and at least one membran...  
WO/2016/084000A1
An auxiliary safety system for controlling the attitude of an aircraft (1) provides sensors placed on the aircraft (1) which identify stalling and/or other critical flying conditions that are imminent and/or have occurred, an electronic ...  
WO/2016/053452A1
A method of controlling noise of an aircraft includes storing a plurality of predefined noise modes; receiving a selection of a selected noise mode from the plurality of predefined noise modes, the selected noise mode identifying at leas...  
WO/2016/037035A1
An airspeed estimation system of an aircraft includes an electronic airspeed rate modeler unit configured to output an estimated airspeed rate signal indicating an estimated airspeed rate of the aircraft. The estimated airspeed rate sign...  
WO/2015/130360A3
A system for enhancing vision inside an aircraft cockpit (10) includes a primary display system (34) configured to receive the signals related to flight data (33) and display visual representations based on the flight data (33). The syst...  
WO/2015/126513A2
Peripheral vision hover drift cueing methods, systems and computer readable media are disclosed. For example, a system can include one or more sensors, and a peripheral vision hover drift cueing controller coupled to the one or more sens...  

Matches 1 - 50 out of 658