CN216546705U - Intelligent aircraft based on MCU chip - Google Patents

Intelligent aircraft based on MCU chip Download PDF

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Publication number
CN216546705U
CN216546705U CN202220161158.7U CN202220161158U CN216546705U CN 216546705 U CN216546705 U CN 216546705U CN 202220161158 U CN202220161158 U CN 202220161158U CN 216546705 U CN216546705 U CN 216546705U
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mcu chip
aircraft
module
display screen
aircraft body
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CN202220161158.7U
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Chinese (zh)
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王文凯
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Dongguan Kude Intelligent Technology Co ltd
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Dongguan Kude Intelligent Technology Co ltd
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Abstract

The utility model discloses an intelligent aircraft based on an MCU (microprogrammed control Unit) chip, which comprises an aircraft body, wherein an MCU chip control board is installed inside the aircraft body, a motor driving and controlling module is integrally and electrically connected onto the MCU chip control board, and a loading display screen and a loading loudspeaker are rotatably installed on a rotating bracket through a rotating motor; the display screen and the loudspeaker can be carried through the loading of the aircraft body, and the display angle of the display screen can be adjusted to adapt to the observation angle required by the ground, so that the unmanned aerial vehicle has better adjusting effect when hovering display and broadcasting work is carried out; in addition, the control mode of the unmanned aerial vehicle aircraft is switched between a short distance and a long distance, and meanwhile, the WAP communication module, the WIFI communication module and the storage card reading module enable the displayed and played content to be set in a mode of respectively adopting WAP communication, WIFI communication and storage card storage so as to adapt to the display and broadcast work of the unmanned aerial vehicle under different requirements.

Description

Intelligent aircraft based on MCU chip
Technical Field
The utility model relates to the technical field of intelligent aircrafts, in particular to an intelligent aircraft based on an MCU chip.
Background
An intelligent aircraft, also called an unmanned aerial vehicle, abbreviated in english as UAV, is an unmanned aerial vehicle operated by means of a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer; the Micro Control Unit (MCU), also called single chip microcomputer or single chip microcomputer, properly reduces the frequency and specification of the CPU, and integrates the peripheral interfaces of memory, counter, USB, A/D conversion, UART, PLC, DMA, etc., even LCD drive circuit on a single chip to form a chip-level computer for different combined control in different application occasions.
With the application of the unmanned aerial vehicle aircraft in different occasions, the unmanned aerial vehicle can be put on the audio and video accessory in practical occasions, and the work of auxiliary work and broadcasting can be performed by matching with the hovering flight mode of the unmanned aerial vehicle, but the display angle of the display screen is difficult to change through the flight mode of the aircraft; meanwhile, the short-distance control of the conventional aircraft adopts a WIFI or Bluetooth communication mode, the effective transmission distance is limited, and the communication transmission and storage modes of the content broadcasted by the display screen and the loudspeaker on the aircraft are limited, so that an intelligent aircraft based on the MCU chip is required to be provided.
Disclosure of Invention
The utility model aims to provide an intelligent aircraft based on an MCU chip to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
an intelligent aircraft based on an MCU chip comprises an aircraft body, wherein an MCU chip control board is installed inside the aircraft body, a motor driving and controlling module is electrically connected to the MCU chip control board in an integrated mode, a rotating support is rotatably installed at the bottom of the aircraft body, a loading display screen and a loading horn are installed at the bottom of the rotating support, a rotating motor for driving the rotating support to rotate is installed at the bottom of the aircraft body, and the motor driving and controlling module is electrically connected to a stepping control end of the rotating motor;
still integrated electric connection has WAP communication module and WIFI communication module, flight control module and display screen drive plate and audio drive board on the MCU chip control panel, flight control module and display screen drive plate and audio drive board all connect in WAP communication module and WIFI communication module through MCU chip control panel, load the display screen and load loudspeaker and be controlled by display screen drive plate and audio drive board respectively.
Preferably, a plurality of groups of flight wings are installed on the aircraft body, and a floor support for supporting the aircraft body is installed at the bottom of the aircraft body.
Preferably, the bottom fixedly connected with mount of aircraft body, the rotation support rotates to be connected in the bottom of mount, the output shaft that rotates the motor and install in the lateral part of mount and rotate the motor connects in the upper portion of rotating the support.
Preferably, the flight control module is electrically connected to the control ends of the flight wing motors of the plurality of sets of flight wings.
Preferably, load the loudspeaker and be provided with two sets ofly and be located the both sides of loading the display screen respectively, a plurality of groups pilot lamp are still installed to the bottom of aircraft body.
Preferably, the MCU chip control board is further integrated with a storage card reading module and a rechargeable power supply module, and the storage card reading module is electrically connected to the MCU chip control board.
Compared with the prior art, the utility model has the beneficial effects that:
through the design of the rotating motor, the motor driving and controlling module, the fixing frame, the rotating support, the loading display screen, the loading loudspeaker and other structures, the display screen and the loudspeaker can be carried through the loading of the aircraft body, and meanwhile, the display angle of the display screen can be adjusted to be matched with the observation angle required by the ground, so that the unmanned aerial vehicle has a better adjusting effect when hovering display and broadcasting work is carried out; in addition, the flight control module of the unmanned aerial vehicle aircraft adopts two communication modes, namely a WAP communication module and a WIFI communication module, so that the control modes of the unmanned aerial vehicle aircraft are switched at short distance and long distance, and meanwhile, the WAP communication module, the WIFI communication module and the storage card reading module are used for setting the contents displayed and played in a mode of WAP communication, WIFI communication and storage card storage respectively, so that the unmanned aerial vehicle can display and broadcast under different requirements in adaptation.
Additional features and advantages of the utility model will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the utility model. The objectives and other advantages of the utility model will be realized and attained by the structure particularly pointed out in the written description and drawings.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a system block diagram of the internal control mode of the aircraft body according to the utility model;
FIG. 3 is a circuit diagram of a display screen driver board according to the present invention;
FIG. 4 is a circuit diagram of a WAP communication module of the present invention;
FIG. 5 is a schematic circuit diagram of the motor control module of the present invention;
FIG. 6 is a circuit diagram of the memory card reading module according to the present invention.
In the figure: 1. an aircraft body; 2. a flying wing; 3. a floor stand; 4. MCU chip control panel; 5. a fixed mount; 6. rotating the bracket; 7. loading a display screen; 8. loading a horn; 9. rotating the motor; 10. a display screen driving board; 11. an audio driver board; 12. an indicator light; 13. a flight control module; 14. a WAP communication module; 15. a motor driving and controlling module; 16. a storage card reading module; 17. a rechargeable power supply module; 18. and a WIFI communication module.
Detailed Description
The same reference numbers in different drawings identify the same or similar elements; it should be further understood that terms such as "first," "second," "third," "upper," "lower," "front," "back," "inner," "outer," "end," "portion," "section," "width," "thickness," "zone," and the like, as used herein, are merely used for convenience in referring to the figures and to aid in describing the utility model, and are not intended to limit the utility model.
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, the present invention provides an embodiment:
an intelligent aircraft based on an MCU chip comprises an aircraft body 1, wherein an MCU chip control board 4 is installed inside the aircraft body 1, a motor driving and controlling module 15 is electrically connected to the MCU chip control board 4 in an integrated mode, a circuit schematic diagram of the motor driving and controlling module 15 is shown in fig. 5, a rotating support 6 is rotatably installed at the bottom of the aircraft body 1, a loading display screen 7 and a loading loudspeaker 8 are installed at the bottom of the rotating support 6, a rotating motor 9 for driving the rotating support 6 to rotate is installed at the bottom of the aircraft body 1, and the motor driving and controlling module 15 is electrically connected to a stepping control end of the rotating motor 9;
still integrated electrically connected has WAP communication module 14 and WIFI communication module 18, flight control module 13 and display screen drive plate 10 and audio drive plate 11 on the MCU chip control panel 4, flight control module 13 and display screen drive plate 10 and audio drive plate 11 all connect in WAP communication module 14 and WIFI communication module 18 through MCU chip control panel 4, load display screen 7 and load loudspeaker 8 and be controlled by display screen drive plate 10 and audio drive plate 11 respectively.
The circuit schematic diagrams of the WAP communication module 14 are respectively shown in fig. 4, and the WIFI communication module 18 is a common control mode for controlling a conventional short-distance unmanned aerial vehicle, and is not disclosed nor described again here; the WAP communication module 14 is disposed on the aircraft body 1, and a ground controller of the aircraft is also provided with a WAP communication function, so that information at a longer distance can be transmitted to the aircraft body 1 through a WAP communication satellite in a network uploading manner.
The aircraft comprises an aircraft body 1, a plurality of groups of flight wings 2, and a landing support 3 for supporting the aircraft body 1, wherein the landing support is arranged at the bottom of the aircraft body 1; the flight control module 13 is electrically connected to the control ends of the flight wing motors of the plurality of sets of flight wings 2.
The bottom of the aircraft body 1 is fixedly connected with a fixed frame 5, the rotating support 6 is rotatably connected to the bottom of the fixed frame 5, the rotating motor 9 is mounted on the side part of the fixed frame 5, and the output shaft of the rotating motor 9 is connected to the upper part of the rotating support 6; the bottom rotating bracket 6 is controlled to rotate from the side part of the fixed frame 5 by the installation mode of the rotating motor 9, so that the rotating angles of the loading display screen 7 and the loading loudspeaker 8 are adjusted or the loading loudspeaker 8 rotates back and forth circularly.
When the unmanned aerial vehicle is used specifically, through the design of the structures such as the rotating motor 9, the motor driving and controlling module 15, the fixing frame 5, the rotating support 6, the loading display screen 7, the loading loudspeaker 8 and the like, the display screen and the loudspeaker can be carried through the loading of the aircraft body 1, and meanwhile, the display angle of the display screen can be adjusted to be matched with the observation angle required by the ground, so that the unmanned aerial vehicle has a better adjusting effect when hovering display and broadcasting work are carried out; in addition, the flight control module 13 of the unmanned aerial vehicle aircraft adopts two communication modes, namely a WAP communication module 14 and a WIFI communication module 18, so that the control modes of the unmanned aerial vehicle aircraft can be switched between a short distance and a long distance, and meanwhile, the WAP communication module 14, the WIFI communication module 18 and the storage card reading module 16 enable displayed and played contents to be set in a mode of WAP communication, WIFI communication and storage card storage respectively, so that the unmanned aerial vehicle can display and broadcast under different requirements in a matching mode.
The loading horns 8 are provided with two groups and are respectively positioned at two sides of the loading display screen 7, and a plurality of groups of indicator lamps 12 are further arranged at the bottom of the aircraft body 1; the MCU chip control board 4 is also integrated with a storage card reading module 16 and a rechargeable power supply module 17, and the storage card reading module 16 is electrically connected with the MCU chip control board 4; a circuit schematic of the memory card reading module 16 is shown in fig. 6.
The control mode of the present application document is automatically controlled by a controller, and the control circuit of the controller can be realized by simple programming of a person skilled in the art, which belongs to the common knowledge in the field, and the present application document is mainly used for protecting a mechanical device, so the present application document does not explain the control mode and the circuit connection in detail, and the device supplies power by an internal power supply or an external power supply.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides an intelligent aircraft based on MCU chip, includes aircraft body (1), its characterized in that: the aircraft is characterized in that an MCU chip control board (4) is installed inside the aircraft body (1), a motor driving and controlling module (15) is electrically connected to the MCU chip control board (4) in an integrated mode, a rotating support (6) is installed at the bottom of the aircraft body (1) in a rotating mode, a loading display screen (7) and a loading loudspeaker (8) are installed at the bottom of the rotating support (6), a rotating motor (9) for driving the rotating support (6) to rotate is installed at the bottom of the aircraft body (1), and the motor driving and controlling module (15) is electrically connected to a stepping control end of the rotating motor (9);
still integrated electric connection has WAP communication module (14) and WIFI communication module (18), flight control module (13) and display screen drive plate (10) and audio drive board (11) on MCU chip control panel (4), flight control module (13) and display screen drive plate (10) and audio drive board (11) all connect in WAP communication module (14) and WIFI communication module (18) through MCU chip control panel (4), load display screen (7) and load loudspeaker (8) and be controlled by display screen drive plate (10) and audio drive board (11) respectively.
2. The intelligent aircraft based on MCU chip of claim 1 characterized in that: the aircraft is characterized in that a plurality of groups of flight wings (2) are installed on the aircraft body (1), and a floor support (3) used for supporting the aircraft body (1) is installed at the bottom of the aircraft body (1).
3. The intelligent aircraft based on MCU chip of claim 1 characterized in that: the bottom fixedly connected with mount (5) of aircraft body (1), rotate support (6) and rotate and connect in the bottom of mount (5), rotate motor (9) and install in the lateral part of mount (5) and the output shaft of rotating motor (9) and connect in the upper portion of rotating support (6).
4. The intelligent aircraft based on MCU chip of claim 2 characterized in that: the flight control module (13) is electrically connected to the control ends of the flight wing motors of the plurality of groups of flight wings (2).
5. The intelligent aircraft based on MCU chip of claim 1 characterized in that: load loudspeaker (8) and be provided with two sets ofly and be located the both sides of loading display screen (7) respectively, a plurality of groups pilot lamp (12) are still installed to the bottom of aircraft body (1).
6. The intelligent aircraft based on MCU chip of claim 1 characterized in that: the MCU chip control board (4) is further integrated with a storage card reading module (16) and a rechargeable power supply module (17), and the storage card reading module (16) is electrically connected to the MCU chip control board (4).
CN202220161158.7U 2022-01-21 2022-01-21 Intelligent aircraft based on MCU chip Active CN216546705U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220161158.7U CN216546705U (en) 2022-01-21 2022-01-21 Intelligent aircraft based on MCU chip

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220161158.7U CN216546705U (en) 2022-01-21 2022-01-21 Intelligent aircraft based on MCU chip

Publications (1)

Publication Number Publication Date
CN216546705U true CN216546705U (en) 2022-05-17

Family

ID=81561808

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220161158.7U Active CN216546705U (en) 2022-01-21 2022-01-21 Intelligent aircraft based on MCU chip

Country Status (1)

Country Link
CN (1) CN216546705U (en)

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