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WO/2023/282124A1 |
A drone 10 comprises: a detection unit 12 that, after a flying vehicle is located over a structure specified as a destination, detects, on the basis of an image of a site including the structure captured by the flying vehicle, the struct...
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WO/2023/277847A1 |
The present invention relates to a console (C) provided in air vehicles; at least one control stick (2) located on the console (C), providing mission input to the air vehicle by the user; at least one bracket (3) allowing the control sti...
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WO/2023/274914A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2023/277723A1 |
The claimed invention relates to aviation and concerns command posts for manually controlling an aircraft, in particular a single-rotor helicopter. In one of the possible design embodiments, the invention is envisaged as follows. A yoke ...
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WO/2023/274913A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2023/276640A1 |
Provided is a flying object control system comprising an area-forming part that forms a prescribed area relative to a grip, a detection unit that detects a displacement of the prescribed area formed by the area-forming part, and a contro...
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WO/2023/276454A1 |
The control device according to the present invention comprises a processor and a memory that is connected to or built into the processor. The processor carries out, when the processor causes a rotary drive device on which a distance mea...
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WO/2022/263777A1 |
The invention relates to an aircraft flight compensator comprising a friction module (8) that has variable friction and is coupled on one side to a drive shaft (11) and on the other side to an output shaft (13) via a kinematic chain (12)...
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WO/2022/259631A1 |
A moving body according to one aspect of the present technology comprises a body part, a notification part, and a notification control part. The notification part is provided to the body part. By controlling the operation of the notifica...
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WO/2022/259799A1 |
A control device that comprises a processor and a memory that is connected to or housed in the processor. The processor: obtains the vertical position of a marker detected by an optical sensor mounted on a flight vehicle, for a marker th...
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WO/2022/260931A1 |
A jam free linear actuator system includes a linear electro-mechanical actuator configured to actuate a component; a disengagement mechanism configured to disengage components of the linear electro-mechanical actuator in an event of a ja...
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WO/2022/254162A1 |
The invention relates to an aircraft flight compensator control system including a motor (3) and a variable-friction actuator (6) coupled to the motor and to an output shaft (8). The variable-friction actuator includes a variable-frictio...
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WO/2022/251598A1 |
Systems, devices, and methods for an aircraft autopilot guidance control system (100, 300) for guiding an aircraft having a body, the system comprising: a processor (101) configured to determine if a yaw angle difference and a pitch angl...
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WO/2022/249319A1 |
In this invention, a management server 2 calculates, on the basis of the weight of articles included in each of a plurality of orders, a total weight of the plurality of articles to be loaded on a UAV1 and compares the calculated total w...
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WO/2022/243113A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated such that it sequentially adopts a plurality of different partial load sharing modes in a time variable manner, which provide for...
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WO/2022/243112A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated in at least one normal operation mode such that it provides for load sharing across electrical power sources (A, B, C, D) with re...
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WO/2022/216747A9 |
Some embodiments relate to an electro-mechanical actuator that includes a screw, structurally segregated (split) housings, first and second nuts coupled to the screw, a sensor assembly, a plurality of motors, and a controller. The first ...
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WO/2022/230561A1 |
The present invention provides a float that provides a higher degree of freedom in the installation location of an air hole for reducing deformation of the float body associated with the expansion or contraction of an internal gas due to...
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WO/2022/226012A1 |
An actuator transfer assembly comprising an actuator (18), a driven object (16, 116), a pushrod (19) or shaft (119), a disconnect housing (24, 124), a transfer member (50) movable relative to the housing from a first position in mechanic...
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WO/2022/215266A1 |
[Problem] To provide a flight vehicle landing method and the like, for a directional flight vehicle, whereby it is possible to improve the landing performance of the directional flight vehicle by turning in a nose direction with a good b...
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WO/2022/212247A1 |
In an aspect a system for fly-by-wire flight control configured for use in electric aircraft includes at least a sensor, wherein the sensor is communicatively connected a pilot control and configured to detect a pilot input from the pilo...
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WO/2022/209398A1 |
[Problem] To provide: an information processing method with which a flight route for a flying body can be generated by a simple operation; an information processing device; a computer-readable medium; and an imaging system. [Solution] An...
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WO/2022/208491A1 |
This monitoring plan creation device: divides monitoring map information corresponding to a monitored area indicating the entire region monitored by an unmanned vehicle into small areas, and sets the initial values of time intervals at w...
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WO/2022/210691A1 |
The present invention provides a flight device that can measure the weight of a transported object accurately with a simple configuration. A flight device 10 is provided with a rotor 11, a motor 12, a flight sensor 13, a power conversion...
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WO/2022/196597A1 |
[Problem] Flares are used as means for jamming guided missiles that employ infrared rays in terminal guidance; however, in the case of infrared sensors having simultaneous multi-target processing capabilities, there is a possibility that...
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WO/2022/196515A1 |
[Problem] To provide a flight control system with which it is possible to perform safe manual steering of a flying body without requiring advanced steering technology. [Solution] The flight control system according to the present inventi...
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WO/2022/182587A1 |
The present disclosure relates generally to control systems, and in particular apparatus, methods, and systems for controlling flights remotely or onboard the vehicle. More specifically, the present disclosure describes embodiments of a ...
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WO/2022/181176A1 |
An attitude control device according to one aspect of the present invention comprises a detection unit that detects the inclination of a flying body, and a notification unit that executes a process of notifying a passenger according to t...
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WO/2022/175099A1 |
The present invention relates to an integrated controller unit (10) for controlling at least one engine motor (26) and at least one servo motor (28), comprising a power link section (12) for connecting the controller unit (10) to an exte...
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WO/2022/176446A1 |
The flight vehicle according to an embodiment of the present technology is provided with a recording unit, a detection unit, and a reproduction unit. The recording unit records flight parameters during flight in which a sensor anomaly is...
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WO/2022/175118A1 |
An inceptor apparatus (30a; 30b) for an aircraft comprises a primary inceptor member (32a; 32b) provided in the form of a stick member having a grip portion, at which the stick member can be gripped by a pilot's hand, and a secondary inc...
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WO/2022/175106A1 |
A flight control system (10) for an aircraft comprises a flight control computer system (12), which is connected via an electronic or optoelectronic bus system (22) with a plurality of bus nodes (14, 16, 18, 20), which each are configure...
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WO/2022/171215A1 |
A method for a carrying structure deformation control according to this invention lies in that an auxiliary structure connected to a frame is created in parallel with a basic carrying structure, both the structures are connected one to a...
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WO/2022/153784A1 |
A drone control system (100) comprises a destination determination unit (114) and a movement instruction unit (115). The destination determination unit (114) determines the destination of a drone (101) from a plurality of standby locatio...
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WO/2022/153392A1 |
Provided is a system in which an uncrewed aircraft performs autonomous flight so as to follow the outer wall of a structure such as a tunnel. This self-position estimation system includes: a vertical-section measurement data acquisitio...
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WO/2022/153391A1 |
Provided is a system for estimating the location of an unmanned aerial vehicle in the case when autonomous flight is carried out by the unmanned aerial vehicle within the interior space of a structure such as a tunnel. In the present i...
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WO/2022/117960A9 |
The invention relates to a method for controlling an engine, a device for controlling an engine and an aircraft, the method comprising the steps of determining (202) a first intensity Kp, representing a stiffness, according to a physical...
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WO/2022/153390A1 |
Provided is a system for estimating the position of an uncrewed aircraft when the uncrewed aircraft flies within the internal space of a structure, such as a tunnel, having an internal surface on which feature points are difficult to ide...
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WO/2022/148749A1 |
The invention relates to a takeoff and landing pad (22) which can for example be located on the roof of a high-rise building and is equipped with a fan arrangement (2) which draws in air and expels it upwards and in so doing acts against...
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WO/2022/147284A1 |
According the present invention, air velocity and speed of sound which can be used to estimate air temperature can be measured from a sonic anemometer system attached to an airborne platform. Using multiple sonic emitters and receivers c...
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WO/2022/145045A1 |
[Problem] To provide a flying object control method. [Solution] Provided is a method for controlling, on the basis of prescribed information, the body orientation of a flying object so as to be oriented in a direction in which flying eff...
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WO/2022/137067A1 |
The present disclosure provides a modular and scalable platform for the development of land and/or flying multi-purpose manned and unmanned vehicles. The platform including a plurality of parts is provided for structural support, wherein...
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WO/2022/140077A1 |
A jam free dual redundant actuator lane changer system includes a primary lane system and a secondary lane system. The primary lane system is configured to provide actuation of a component during a normal operation while the secondary la...
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WO/2022/132412A1 |
An apparatus comprises an aerial drone with a coherent radar system on a chip that operates in the terahertz range, the chip being in physical contact with the drone and configured to conduct a noninvasive scan of a target in a line of s...
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WO/2022/122570A1 |
User-actuatable paddle button, said button comprising first and second paddles (16, 18) mechanically attached to each other only by means of a detachable zone (20) to ensure that the first and second paddles can only be moved at the same...
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WO/2022/123962A1 |
Provided is a control device comprising: a product sales device information receiving unit for receiving, from a product sales device for selling products to users, product sales device information pertaining to the product sales device ...
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WO/2022/119913A1 |
A delivery device to deliver a product from an aerial location includes a body defining a payload holding region. The delivery device may further include a coupling mechanism configured to couple the body to a primary vehicle. The delive...
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WO/2022/112046A1 |
The invention relates to a device comprising: - a mount (10), - a frame (20) mounted so as to rotate relative to the mount; - a control arm (40) mounted so as to rotate on the frame (20); a roll spider (80) mounted so as to rotate on the...
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WO/2022/107758A1 |
An available work storage unit 13 stores machinery/equipment 4 on which an unmanned aircraft 2 is to carry out work, and work content which can be carried out on the machinery/equipment 4. A work content acquisition unit 14 acquires mach...
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WO/2022/107761A1 |
In an embodiment, a wireless LAN is installed in a factory. Mechanical equipment 4 of the factory includes a short-range wireless communication unit 41. An unmanned aerial vehicle 2 stores segmented regions of a three-dimensional map or ...
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