WO2017208199A1 - Caméra de super drone vtol amphibie dans un boîtier mobile (boîtier de téléphone) à multiples modes de vol aérien et aquatique pour capturer des vues de réalité virtuelle panoramiques, selfie et vidéo interactive - Google Patents
Caméra de super drone vtol amphibie dans un boîtier mobile (boîtier de téléphone) à multiples modes de vol aérien et aquatique pour capturer des vues de réalité virtuelle panoramiques, selfie et vidéo interactive Download PDFInfo
- Publication number
- WO2017208199A1 WO2017208199A1 PCT/IB2017/053270 IB2017053270W WO2017208199A1 WO 2017208199 A1 WO2017208199 A1 WO 2017208199A1 IB 2017053270 W IB2017053270 W IB 2017053270W WO 2017208199 A1 WO2017208199 A1 WO 2017208199A1
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- WIPO (PCT)
- Prior art keywords
- camera
- video
- user
- case
- headset
- Prior art date
Links
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/26—Ducted or shrouded rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/40—Modular UAVs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/31—Supply or distribution of electrical power generated by photovoltaics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
Definitions
- the present invention relates a phone case. More specifically, the present invention relates to phone case which has a drone and a camera in the phone case.
- the conventional phone case usually meant for protecting the phone.
- the objective of the present invention to utilize a drone and a camera in the phone case and helping the user to capture videos.
- a mobile case system comprising: a real time broad cast stream recording; an unmanned aerial vehicle; a camera stabilization device; a camera movement device configured move the camera; one or more on board cameras for providing a realtime first-person video and a real-time first-person view and normal footage video recording and 360-degree panoramic video recording used for virtual reality views and interactive video; a video transmitter and receiver device configured to perform high definition low latency real time video downlink, wherein the video transmitter and receiver device is a high power, high gain, and ultrahigh frequency device; a one way and two way telemetry device; a live broadcast device; a headset configured to enable the real-time first-person video and a real-time first-person view; a public database for viewing flight or dive activity; plurality of software for licensing videos with a watermarked preview; software for autonomously extracting usable footage and compiling the usable footage into a video montage synced to music; Onboard or separate software for stitching photos to form a modified photo; and on board or
- FIG. 1 is a close up of the isometric view of the first example of the present invention.
- FIG. 2 is a close up of the front view of the first example of the present invention.
- FIG. 3 is a close up of the back view of the first example of the present invention.
- FIG. 4 is a close up of the right view of the first example of the present invention.
- FIG. 5 is a close up of the left view of the first example of the present invention.
- FIG. 6 is a close up of the top view of the first example of the present invention.
- FIG. 7 is a close up of the bottom view of the first example of the present invention.
- FIG. 8 is a close up of the isometric view of the second example of the present invention.
- FIG. 9 is a close up of the isometric view of the third example of the present invention.
- FIG. 10 is a close up of the isometric view of the fourth example of the present invention.
- FIG. 11 is a close up of the isometric vie of the fifth example of the present invention.
- FIG. 12 is a close up of the front view of the fifth example of the present invention.
- FIG. 13 is a close up of the back view of the fifth example of the present invention.
- FIG. 14 is a close up of the top vie of the fifth example of the present invention.
- FIG. 15 is a close up of the bottom view of the fifth example of the present invention.
- FIG. 16 is a close up of the isometric view of the sixth example of the present invention.
- FIG. 17 is a close up of the isometric view of the seventh example of the present i vention
- FIG. 18 is a close up of the isometric view of the eighth example of the present invention.
- FIG. 19 is a close up of the isometric view of the ninth example of the present invention.
- FIG. 1 illustrates a mobile case lQQ,an unmanned aerial device 105, according to an example embodiment.
- the unmanned vehicle 105 also referred herein to as the drone 105 may be used for photography and video capturing.
- the unmanned device may be single axis or coaxial motor system and may be propelled by a direct drive, for example when propellers 120 are directly attached to a motor, or by belts and pulleys, chains and sprockets, magnets, and/or rigid links, where the propellers 120 may be indirectly linked to the motor shaft.
- the motors may be powered by electricity or high pressure fluid, including gas.
- the device 100 may further include a tilt fuselage device, a tilt wing device, and a tilt motor device. Additionally, the device 100 may include a battery. The shape of the battery may conform to the interior shape of the device 100 to maximize the use of the internal volume of the device 100.
- the device 100 may include through-wail wire and antenna feedthroughs which may be sealed to prevent water leakage. The two-way telemetry transmitter may send GPS coordinates back to the operator in the case of the device 100 is lost.
- the device 100 may include a cooling system.
- the cooling system may be selected from ventilation cooling units, heat sink cooling units, liquid cooling units, and fan cooling units.
- the device 100 may further include a detachable skin or shell for impact absorption and scratch protection.
- device 100 may include lights for clear camera vision or lights for signalling, such as for the reception of a command, warning messages, and/or status reports.
- the device 100 may utilize a lap counter that may function by communication between a sensor and an on board transponder.
- the multimotor vehicle may utilize a quick connect payload system which may operate by a click in place, snap in place, screw in place, or slide in place mechanism.
- the device 100 may comprise at least one claw for grasping instruments used to observe or capture specimens, handle specimens, and transportation.
- the device 100 may comprise an inclined launching platform. In example embodiments, device 100 may be launched at an obtuse angle to the ground for expedient take-off.
- the device 100 may further include a deployable parachute i case of the failure of the device 100 when airborne.
- the multimotor vehicle may include devices for internally housing or externally attaching a payload of goods.
- the device 100 may comprise a motorized or pressurized latch mechanism attached onto the payload or payload housing for an impermanent time period.
- the device 100 may comprise an empty internal storage area that may be accessed by a motorized or pressurized hatch.
- the payload may be left at the destination by ways involving the device 100 to descend to an altitude below 15 feet.
- the payload may also be left at the destinatio by a free fall parachute or a guided parachute.
- the device 100 may further include an integrated modular electronics system that may include a central flight control component (including sensors and control parameters), electronic speed controllers, a power distribution harness or board, a telemetry module, a radio control receiver, and a video transmitter.
- the power distribution board may serve as the platform upon which the other electronics components may be linked to each other and the power distributio board by numerous pins, soldering connections, and a minimal amount of wires.
- the various components may be arranged to compact within a single board that can be serviced with hardware updates. Individual electronics components may be substituted if broken or outdated, simply by disordering a one part solder connection or detaching a two part pin connectio or plug connection.
- increased battery 130 capacity may be desired for endurance flights.
- the sw r appable hatches may accommodate a battery 130 within a waterproof shell, and may be substituted with the hatch to fasten the described dual purpose battery hatch-module.
- the device 100 may further include a radio control and video systems that may run on different very high frequency (30-300 MHz), ultrahigh frequency (300 MHz-3 GHz), or super high frequency (3-30 GHz) channels.
- the very high and ultra-high frequency categories offer the best obstacle penetration and may be used with high gain (10-30 dBic) antennas and high power (800 mw-10 w) transmitter/receiver sets for wireless underwater communication and long range aerial communication.
- the device 100 may include onboard or separate media editing systems for virtual reality views, interactive video, or stitched photos. If the onboard media editing systems are used, a transformed footage may be downlinked to the operator in real time with low latency. When low latency footage cannot be achieved, the onboard media editing systems may transform the media before or shortly after landing. If onboard media editing systems are not implemented, post-capture media editing methods may be applied.
- the plurality of motors 115 and propellers 120 may include ducted propellers 120, such as multi-blade ducted fans, fixed pitch propellers, controllable pitch propellers, two- position propellers 120, full feathering propellers 120, and tilted propellers 120.
- ducted propellers 120 such as multi-blade ducted fans, fixed pitch propellers, controllable pitch propellers, two- position propellers 120, full feathering propellers 120, and tilted propellers 120.
- the plurality of motors 115 and propellers 120 may include two motors 115 and propellers 120, three motors 115 and propellers 120, four motors 115 and propellers 120, five motors 115 and propellers 120, and six motorsllS and propellers.
- at least one of the plurality of motors 115 and propellers 120 is located on a foldable wing, the foldable wing folding in a ground mode and unfolding in a flight mode.
- the motor 115 may be a solar turbine powered master impeller motor disposed centrally in the device 100.
- the solar turbine powered master impeller motor may include an electric-drive impeller.
- the electric-drive impeller may be contained in a compression chamber and may have an axis of rotation oriented perpendicularly to an axis of the device 100.
- the solar turbine powered master impeller motor 115 may be powered by a solar film.
- the solar film may be integrated on an upper surface of the device, a lower surface of the device 100, and the at least one wing of the device.
- the solar turbine powered master impeller motor 115 may be further pow d ered by the electrical pow r er storage device.
- the device 100 may have a propeller protection system.
- the propeller protection system may include a wing tip folding mechanism.
- the propeller protection system may fully or partially surrounds any type of propellers, such as self-tightening fixed pitch propellers and variable pitch propellers.
- the device 100 may include a surface skidding material platform and a landing system.
- the landing system may conform to a landing surface.
- the device 100 may include one or more control surfaces selected from a group comprising: a rudder, an aileron, a flap, and elevator.
- the device 100 may be operable to perform an automatic landing and an automatic takeoff.
- the device 100 further includes a ballast.
- the ballast may be a permanently fixed ballast or a detachable ballast.
- the device 100 may include an onboard air compressor, an onboard electrolysis system, at least one waterproof through-body wire or antenna feed-through.
- the device 100 may further include a battery 130.
- a shape of the battery 130 may conform to an interior profile of the modular and expandable waterproof body 125.
- the battery 130 may be a lithium ion polymer (Li-Po or Li-Poly) battery that conforms to the interior profile, and includes a built-in battery charge indicator.
- the battery 130 is used a power bank for a mobile device, the battery 130 is coupled to the solar panel which converts the solar energy and stores in the battery 130.
- the device 100 may include a Global Positioning System (GPS) module, a lost model alert, a cooling device, such as a heat sink, a fan, or a duct, a detachable impact absorbing skin or shell, vision aiding and orientated lights, such as light emitting diodes, one or more hatches, quick connect payloacls, a lap counter for racing, a flat or inclined launch platform or footing, one or more claws with at least one degree of freedom, an apparatus for externally attaching a cargo and internally housing the cargo, a charging station for multiple batteries. Therefore, the device 100 may serve as a vehicle for carrying people or cargos.
- GPS Global Positioning System
- the device 100 may be configured as one of the following: an autonomous vehicle, a multi-blade ducted fan readable electric aircraft, an unscrewed vehicle, a driverless car, a self- driving car, an unmanned aerial vehicle, a drone, a robotic car, a commercial goods and passenger carrying vehicle, a private self-drive vehicle, a family vehicle, a military vehicle, and a law enforcement vehicle.
- the device 100 may be configured to sense environmental conditions, navigate without human input, and perform autopiloting.
- the sensing of the environmental conditions may be performed via one or more of the following: a radar, a lidar, the GPS module, and a computer vision module.
- the processor of the device 100 may be operable to interpret sensory information to identify navigation paths, obstacles, and signage.
- the autonomous vehicle may be also operable to update maps based on sensory input to keep track of a position when conditions change or when uncharted environments are entered.
- the multi-blade ducted fan readable electric car may be propelled by one or more electric motors using electrical energy stored in the electrical pow T er storage device.
- the storage device is used a on the go for the said mobile device, in another embodiment it is used as usb for the mobile phone, in another embodiment it is used for storing the images captured by the camera 110.
- the device 100 may include one or more modules attached to the modular and expandable waterproof body 125.
- the one or more modules may include a waterproof battery module, a turbine, a solar panel, a claw, a camera stabilizatio device, a thermal inspection device, an environmental sample processor, a seismometer, a spectrometer, an osmo sampler, a night vision device, a hollow waterproof module for upgrades, third party gear, and hardware upgrades.
- the battery 130 may be partially or completely modular.
- the electronic speed controllers may be configured to detach from an electronic speed controller stack.
- the video transmitter and the radio control receiver may be removable for upgrade.
- the onscreen display telemetry device may be removable for upgrade.
- the plurality of motors may be removable for upgrade.
- the flight controller may be configured to detach from the power distribution board.
- the cameras 110 for capturing panoramic views may be mounted on a multi-camera spherical rig.
- the multi-camera spherical rig may be mounted onto a camera stabilization device or a fixed mounting device.
- a content captured by the cameras may be combined to create a panoramic video.
- the device 100 is used to record the videos in 4k resolution, the recorded 4k resolution can adapted for live streaming and broadcasting, the videos can be recorded at different resolutions, the resolutions can be adjusted by a user from the mobile device.
- the device 100 is adapted for taking the selfies and aerial view of the user using the device.
- the video transmitter and receiver device of the system may be configured to control one or more of the following: an omnidirectional or directional antenna, a low pass filter, a ninety degree adapter, head tracking and eye tracking to manipulate movement of the camera stabilization device for video capture or live playback, antenna tracking on the ground station or onboard.
- the live broadcast device may include an onboard High Definition Multimedia Input port operable to transmit standard definition, high definition, virtual reality, and interactive video to one or more bystanders.
- the interactive video may be broadcasted on at least one of the following: a screen, a projector, a split screen, a switch screen, and the headset.
- the live broadcast device may further comprise an aerial, ground, and marine vehicle for filming the unmanned device.
- the present disclosure also refers to a collision avoidance, flight stabilization, and multi-rotor control system for an unmanned device.
- the system may be configured as a flying car and may include a flight and dive control device configured to perform one or more of the following: auto level control, altitude hold, return to an operator automatically, return to the operator by manual input, operating auto-recognition camera, monitoring a circular path around a pilot, and controlling autopilot, supporting dynamic and fixed tilting arms.
- the system may further include one or more sensors and one or more cameras configured to control one or more of the following: obstacle avoidance, terrain and Geographical Information System mapping. close proximity flight including terrain tracing, and crash resistant indoor navigation.
- the system may additionally include an autonomous takeoff device, an auto-fly or dive to a destination with at least one manually or automatically generated flight plan, an auto-fly or dive to the destination by tracking monuments, a direction lock, a dual operator control device, a transmitter and receiver control device.
- the transmitter and receiver control device may include one or more antennas. The antennas may be high gain antennas.
- the transmitter and receiver control device may further include a lock mechanism operated by one or more of the following: numerical passwords, word passwords, fingerprint recognition, face recognition, eye recognition, and a physical key.
- the system may further include at least one electronic speed controllers (ESC) selected from a standalone ESC and an ESC integrated into a power distribution board of the unmanned device.
- the ESC may be operable to program a motor spin direction without reconnecting wires by the user via spinning a motor in a predetermined direction, and record an input.
- the device 100 is attached to a mobile device wherein the mobile device is a smart phone, the mobile device is tablet, wherein the mobile device is augmented reality head mounted display, the head mounted display the augmented reality of the fight control and camera pictures, the battery status in the head mounted display.
- the mobile device is a smart phone
- the mobile device is tablet
- the mobile device is augmented reality head mounted display
- the head mounted display the augmented reality of the fight control and camera pictures, the battery status in the head mounted display.
- the device 100 is coupled with a mobile application wherein the mobile application is used to control the unmanned vehicle.
- the application consists of a user interface wherein the user interface receives the information regarding the camera and the flight conditions of the unmanned vehicle.
- the user interface display the first person view and images captured b the device.
- the UI display the available battery present and altitude and manuveours of the unmanned vehicle.
- the system may further include a radio control device operable to control an omnidirectional or directional antenna, antenna tracking on a ground station or onboard the unmanned device tilt, a low- pass filter, ninety degree adapter, a detachable module for RC communication o a channel having a frequency selected from 72 MHz, 75 MHz, 433 MHz, and 1.2/1.3 GHz, adjustable dual rates and exponential values, at least one dial or joystick for controlling the movement of a camera stabilization device, one or more foot pedals, a slider, a potentiometer, and a switch to transition between a flight profile and a dive profile.
- the radio control device may be controlled by stick inputs and motion gestures.
- the radio control device may be further operable to perform automatic obstacle avoidance and automatic manoeuvring around an obstacle when the unmanned device performs a flight in a predetermined direction. For example, when the user wants the unmanned device to fly forwards through obstacles, such as frees, the user needs only to signal the unmanned device to go forwards, and the unmanned device may autonomously dodge through the obstacles. Additionally, the radio control device may be operable to turn on a swarm fol low-me function by instructing a plurality of unmanned devices to follow a single subject and capture a plurality of views of the subject, where different unmanned devices capture different views of the same subject.
- the system may further include a navigation device.
- the navigation device may be configured to enable autonomous flying at low altitude and avoiding obstacles, evaluate and select landing sites in an unmapped terrain, and land safely using a computerized self-generated approach path.
- the system may be configured to enable a pilot aid to help a pilot to avoid obstacles, such as power lines, and select landing sites in unimproved areas, such as emergency scenes, during operating in low-light or low-visibility conditions.
- the system may be configured to detect and maneuver around a man lift during flying, detect high-tension wires over a desert terrain, and enable operation in a near earth obstacle rich environment
- the system may also include a navigation sensor configured to map an unknown area where obstructions limited landing sites and identify level landing sites with approach paths that are accessible for evacuating a simulated casualty.
- the navigation sensor may be configured to build three-dimensional maps of a ground and find obstacles in a path, detect four -inch- high pallets, chain link fences, vegetation, people and objects that block a landing site, enable continuously identifying potential landing sites and develop landing approaches and abort paths. Additionally, the navigation sensor may be configured to select a safe landing site being closest to a given set of coordinates.
- the navigation sensor may include an inertial sensor and a laser scanner configured to look forward and down.
- the navigation sensor may be paired with mapping and obstacle avoidance software, the mapping and obstacle avoidance software may be operable to keep a running rank of the landing sites, approaches and abort paths to enable responding to unexpected circumstances.
- the unmanned device may include a light detection and ranging !idar and an ultrasonic radar sensor.
- the device is used for aerial transportation of device to smaller distance
- the unmanned aerial vehicle is a delivery drone
- the delivery drone is adapted for to transport packages, food or other goods
- the drone can transport medicines and vaccines, and retrieve medical samples, into and out of remote or otherwise inaccessible regions.
- the drone rapidly deliver defibrillators in the crucial few minutes after cardiac arrests, and include livestream communication capability allowing paramedics to remotely observe and instruct on- scene individuals in how to use the defibrillators.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
L'invention concerne un système de boîtier mobile. Le système de boîtier mobile peut comprendre un boîtier pour un dispositif de commande et un casque d'écoute porté par un utilisateur. Le boîtier peut renfermer le dispositif de commande et peut comprendre un corps extensible, des hélices disposées dans le corps extensible, une antenne pour recevoir des signaux provenant d'un dispositif à distance, une batterie, une caméra, un émetteur-récepteur, un dispositif de télémétrie, un processeur en communication avec le dispositif de commande et le dispositif à distance, et un tableau de distribution d'énergie. Le processeur peut recevoir des instructions provenant du dispositif à distance et commander un fonctionnement des hélices sur la base des instructions. Le processeur peut envoyer la vidéo capturée par la caméra à une base de données publique. Le processeur peut suivre une position du casque d'écoute et commander un angle de visualisation de la caméra sur la base de la position du casque d'écoute. Le casque d'écoute peut être conçu pour afficher la vidéo capturée à l'intention de l'utilisateur.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US15/172,673 | 2016-06-03 | ||
US15/172,673 US20160286128A1 (en) | 2002-10-01 | 2016-06-03 | Amphibious vtol super drone camera in a mobile case (phone case) with multiple aerial and aquatic flight modes for capturing panoramic virtual reality views, selfie and interactive video |
Publications (1)
Publication Number | Publication Date |
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WO2017208199A1 true WO2017208199A1 (fr) | 2017-12-07 |
Family
ID=60479327
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/IB2017/053270 WO2017208199A1 (fr) | 2016-06-03 | 2017-06-02 | Caméra de super drone vtol amphibie dans un boîtier mobile (boîtier de téléphone) à multiples modes de vol aérien et aquatique pour capturer des vues de réalité virtuelle panoramiques, selfie et vidéo interactive |
Country Status (1)
Country | Link |
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WO (1) | WO2017208199A1 (fr) |
Cited By (4)
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CN110001985A (zh) * | 2019-04-01 | 2019-07-12 | 苏州臻迪智能科技有限公司 | 一种智能设备 |
EP3919998A1 (fr) * | 2018-11-22 | 2021-12-08 | Lorenz Technology ApS | Procédé pour induire un comportement autonome dans un véhicule sans pilote et unité de communication destinée à être utilisée dans un tel procédé |
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WO2023143460A1 (fr) * | 2022-01-26 | 2023-08-03 | 维沃移动通信有限公司 | Procédé et dispositif de commande d'ensemble de vol, terminal et support de stockage lisible |
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Publication number | Priority date | Publication date | Assignee | Title |
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EP3919998A1 (fr) * | 2018-11-22 | 2021-12-08 | Lorenz Technology ApS | Procédé pour induire un comportement autonome dans un véhicule sans pilote et unité de communication destinée à être utilisée dans un tel procédé |
US11346938B2 (en) | 2019-03-15 | 2022-05-31 | Msa Technology, Llc | Safety device for providing output to an individual associated with a hazardous environment |
CN110001985A (zh) * | 2019-04-01 | 2019-07-12 | 苏州臻迪智能科技有限公司 | 一种智能设备 |
WO2023143460A1 (fr) * | 2022-01-26 | 2023-08-03 | 维沃移动通信有限公司 | Procédé et dispositif de commande d'ensemble de vol, terminal et support de stockage lisible |
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