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WO/2017/022179A1 |
This control unit (11) of an unmanned flying body (1) determines whether or not the unmanned flying body (1) lies outside the visual field range in which an operator can visually observe the unmanned flying body. Upon determining that th...
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WO/2017/022178A1 |
Provided is an unmanned flying body, a flight control method, and a flight control program whereby it is possible to prevent the unmanned flying body from traveling to a place invisible to an operator and to cause the unmanned flying bod...
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WO/2017/022806A1 |
The present invention establishes a technology for accurately landing an in-flight small aircraft at a destination. A landing guide port device 2 is provided with a port ID storage unit 422 and a guiding radio wave transmission control u...
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WO/2017/018267A1 |
The present invention addresses the problem of providing a flight interference device which can prevent a small unmanned aircraft remotely piloted by radio communication from entering a region to be protected, suppress effects on communi...
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WO/2017/013842A1 |
This unmanned flight vehicle (10) comprises: a remaining battery capacity acquisition unit (112) that acquires the remaining capacity of a battery (106); an arrival determination unit (114) that determines, when the unmanned flight vehic...
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WO/2017/013840A1 |
This unmanned flight vehicle (10) comprises: a time measurement unit (101) that acquires the current time instant; a flyable range changing unit (112) that determines a flyable range of the unmanned flight vehicle (10) in accordance with...
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WO/2017/006421A1 |
In the present invention, a drone 1 carrying baggage takes off from a takeoff device 11, and travels to a user's home 20, which is the delivery destination of the baggage, using a GPS system. When the drone 1 approaches the user's home w...
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WO/2017/007524A1 |
A pneumatic artificial muscle (PAM) actuator (100) includes first and second end caps (102-104), an elastic bladder (106) connected to the end caps, and a covering (108) around the elastic bladder and connected to the end caps. At least ...
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WO/2017/001984A1 |
An aircraft comprises an aircraft structure, a flight control surface attached to the aircraft structure, and a local hydraulic power pack disposed proximal to the flight control surface. The local hydraulic power pack is configured to p...
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WO/2017/001898A1 |
The present invention relates to a mission grip system (1) which enables the pilot/copilot to control the critical mission equipment in aircrafts simultaneously, and basically comprises a pilot mission grip (2); a copilot left hand missi...
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WO/2016/206107A1 |
A system for selecting an operation mode of a mobile platform and methods for making and using same. The system can determine a height of the mobile platform and a disparity between first and second images from the perspective of the mob...
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WO/2016/209697A1 |
Embodiments described herein relate to multicopters with separate engines to power each rotor, wherein the multicopters also include with unique controls to guide the multicopter.
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WO/2016/205088A1 |
The invention concerns an improved CCD integration within pilot seat armrests, with benefits including ease and accuracy of CCD use, premium space savings on cockpit consoles, the ability to be retracted when not in use, always remaining...
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WO/2016/200601A1 |
A system and method for improved efficiency of an integrated power and cooling unit, IPCU (100), of an aircraft is disclosed. The IPCU (100) comprises a compressor (104), a starter/generator (106) and at least a cooling turbine (102), al...
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WO/2016/191071A1 |
A barrel cam rudder pedal system is provided. The system includes an outer housing (24) with a chassis assembly (40) carried by the outer housing (24). A barrel cam arrangement (26) is rotationally mounted within an interior space of the...
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WO/2016/178738A1 |
A method for position hold override control of an aircraft includes determining, by a processor, that a position hold mode is enabled to hold the aircraft at a substantially fixed position with respect to a target. The processor receives...
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WO/2016/176545A1 |
A zero droop handle housing (10) comprises a coupling end (11) and an interior void (13); a shaft (20) comprising a first end (21 ) and a second end (22) where the first end is in the housing proximate the coupling end and extends throug...
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WO/2016/175676A1 |
An aircraft having a canard aerodynamic configuration (see fig. 4) comprises a mechanized wing, which is not shown in the drawing, and also a canard foreplane (10) with a servo flap (3), which are pivotally mounted on the axis of rotatio...
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WO/2016/170766A1 |
This light irradiation device is provided with at least one imaging means which images a monitoring region in order to enable continuously irradiating light accurately onto a moving target, at least one projection means which irradiates ...
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WO/2016/164715A1 |
A method of monitoring health of a hydraulic pump includes identifying, from performance data received from a sensor coupled to a hydraulic system, intervals of steady state and transient state operation. Dynamic element indicators are d...
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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...
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WO/2016/154500A1 |
A three stage watercraft for operation in the water as a traditional boat at low speeds in stage one, for operation on the water's surface at mid-range speeds at stage two, and for traveling in ground effect at higher range speeds is dis...
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WO/2016/146398A1 |
The invention relates to a flight control device for an aircraft, comprising a link lever, mechanical means for limiting an angular course of the link lever, first means (4) for generating a force for the return of the link lever about s...
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WO/2016/143255A1 |
This flying body is an unpiloted flying body capable of flying through the air and comprises: a light-emitting device that emits light; a propulsion device that generates propulsive force for flying through the air; an imaging device tha...
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WO/2016/143256A1 |
This flying body is capable of flying through the air and comprises: a propulsion unit that generates propulsive force for flying through the air; a laser light source that irradiates laser light; an imaging unit that images vertically b...
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WO/2016/143235A1 |
Provided is a maneuvering device, comprising: an input device 101 which detects an input operation which instructs a movement of a moving body, and generates input information; a computation device 11 which changes the input information ...
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WO/2016/138173A1 |
Methods of manufacturing and operating a solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to...
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WO/2016/138139A1 |
A solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to...
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WO/2016/121008A1 |
Provided is a flying robot device that does not cause limits to be imposed on flight time and payload as a result of the capacity of a built-in battery, that enables stable continuous flight of a flying robot, and that makes it possible ...
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WO/2016/121072A1 |
Provided is a flying robot device that enables stable continuous flight of a flying robot, that is capable of performing work such as the dispersing of agricultural chemicals from the sky and aerial photography, and in which sudden load ...
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WO/2016/115062A1 |
A stop module halts rotation of a shaft of a rotational drive system when an axial stroke limit is reached without the use of frictional brake plates. The module has a fixed nut and a pawl carrier coaxially mounted on the shaft for axial...
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WO/2016/111741A1 |
A main rotor trim tab retention system includes, a blade housing having flanges separated by a cavity defined between the flanges, and a trim tab assembly. The trim tab assembly includes, a trim tab having an aerodynamic surface, at leas...
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WO/2016/105650A1 |
A device for releasably mounting an autopilot control circuit to a flight control component of an aircraft, includes a frame that holds a component of an autopilot control circuit; a first coupler releasably fastened to the frame and ope...
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WO/2016/100367A1 |
The disclosed embodiments relate to a flight control computer (212) for an aircraft (10). The flight control computer (212) includes an inertial sensor (332)(334) integrated or incorporated within the flight control computer (212).
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WO/2016/094527A1 |
An aircraft (10), a control surface arrangement (14), and a method of assembling an aircraft are disclosed herein. In an exemplary embodiment, the aircraft includes, but is not limited to, an airframe (12), a control surface (16), and a ...
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WO/2016/089067A1 |
The present invention relates to an unmanned vehicle remote control system and method, which enables an unmanned vehicle capable of automatic point-to-point navigation control, such as an unmanned aerial vehicle or an unmanned vessel, to...
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WO/2016/087891A1 |
A screw (20) assembly for an actuator (10) is described comprising: a screw (20); a nut (22) threaded on said screw (20), such that rotation of said screw (20) causes axial movement of said nut (22); a stop located at an end of said scre...
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WO/2016/088086A1 |
The present invention relates to a data concentration unit (1), which is adapted to convert the analog signals coming from various sensors into digital data and to transmit these digital data to the central unit in order to control all i...
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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 ...
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WO/2016/082014A1 |
A flexible flight control system enables conversion from one architecture using one type of inceptor to another architecture using another type of inceptor, through the usage of modular software and hardware pieces with common interfaces...
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WO/2016/083801A1 |
COUPLING A coupling comprising a brake plate (70); a first friction pad(64) operable to be selectively biased against the brake plate (70). In a first mode of operation the first friction pad(64) is biased against the brake plate (70) by...
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WO/2016/079270A1 |
The invention relates to an actuator (4) for a flight control surface (3) of an aircraft, comprising: - a fixed annulus (9, 10) which can be fixed to a fuselage (2) of the aircraft, - an annulus (11) capable of rotating with respect to t...
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WO/2016/079743A1 |
A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which ca...
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WO/2016/076463A1 |
The present invention relates to a device capable of controlling a flying bot and a control method therefor, the device comprising: a communication unit for performing wireless communication with the flying bot; a display unit for displa...
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WO/2016/076586A1 |
A mobile terminal including a display unit; a wireless communication unit configured to wirelessly communicate with a flying object; and a controller configured to receive an input for setting at least one member of a created group of me...
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WO/2016/068354A1 |
The present invention relates to an unmanned aerial vehicle and an automatic target photographing system, and provides an unmanned aerial vehicle comprising: an aerial vehicle; an image photographing unit, installed in the aerial vehicle...
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WO/2016/060720A1 |
The Curtis Protocol, a standardized aircraft control interface, e.g. for aircraft with multiple flight regimes and flight modes, is provided. The Curtis Protocol standardizes the division and selection of aircraft flight regimes and flig...
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WO/2016/059877A1 |
[Problem] To provide a controller that makes it possible to obtain high-precision images by means of a flight vehicle device. [Solution] Provided is a controller for a flight vehicle device that is provided with an imaging device that ca...
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WO/2016/057098A2 |
A drone traffic management system comprising a computer comprising memory means for storing origin coordinates indicating an origin location of a drone, destination coordinates indicating a destination of the drone, and traffic managemen...
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WO/2016/054215A1 |
An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending...
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