CN105912023A - Portable multifunctional unmanned aerial vehicle and control system and control method thereof - Google Patents

Portable multifunctional unmanned aerial vehicle and control system and control method thereof Download PDF

Info

Publication number
CN105912023A
CN105912023A CN201610376546.6A CN201610376546A CN105912023A CN 105912023 A CN105912023 A CN 105912023A CN 201610376546 A CN201610376546 A CN 201610376546A CN 105912023 A CN105912023 A CN 105912023A
Authority
CN
China
Prior art keywords
unmanned plane
main controller
module
plane main
signal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201610376546.6A
Other languages
Chinese (zh)
Other versions
CN105912023B (en
Inventor
王翔
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing Hepu Aviation Technology Co Ltd
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201610376546.6A priority Critical patent/CN105912023B/en
Publication of CN105912023A publication Critical patent/CN105912023A/en
Application granted granted Critical
Publication of CN105912023B publication Critical patent/CN105912023B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Closed-Circuit Television Systems (AREA)
  • Telephone Set Structure (AREA)

Abstract

The invention discloses a portable multifunctional unmanned aerial vehicle (UAV) and a control system and a control method thereof. The UAV comprises a vehicle body composed of a top, a bottom and sides. A spherical crown rotor arm is hinged to the upper end of each side. For each spherical crown rotor arm, the middle is a circular cavity in which a rotor mechanism is arranged, the top spherical crown of the spherical crown rotor arm is a rotor mechanism protection cover, and the rotor mechanism protection cover is detachably connected to the spherical crown rotor arm. The top of the vehicle body is equipped with a spherical crown top lamp. The bottom of the vehicle body is equipped with a spherical crown base, and the bottom of the spherical crown base is a plane. The front side of the vehicle body is equipped with a camera and recorder. The rear side of the vehicle body is equipped with a display. The left and right sides of the vehicle body are each equipped with a loudspeaker. The whole UAV is spherical in a folded state. The UAV is small and easy to carry, and can achieve the functions of aerial shooting, lighting and video playing.

Description

A kind of portable multi-function unmanned plane and control system thereof and control method
Technical field
The present invention relates to unmanned plane field, refer in particular to a kind of portable multi-function unmanned plane and control system thereof and control method.
Background technology
Universal along with unmanned plane, increasing people likes taking photo by plane with unmanned plane, and unmanned plane is taken photo by plane conveniently, and shooting personnel need not mobile scenery just to carry out multi-faceted shooting, and uses unmanned plane also to can overcome the disadvantages that mobile phone and the constant defect of camera self-timer.And present unmanned plane, volume is big, not readily portable;And present unmanned plane price of taking photo by plane is high, just can be only applied to take photo by plane;Function singleness.
Summary of the invention
It is an object of the invention to: for the problem of above-mentioned existence, it is provided that a kind of portable multi-function unmanned plane and control system thereof and control method, this unmanned plane volume is little, it is simple to carry, and this unmanned plane is capable of taking photo by plane, illuminates, video playback.
The technical solution used in the present invention is as follows:
The invention discloses a kind of portable multi-function unmanned plane, it includes that body, described body include end face, bottom surface and all around four sides, and upper end, described each side is hinged with a ball-crown body rotor arm;Being circular cavity in the middle part of this ball-crown body rotor arm, be provided with rotor mechanism in cavity, the top ball-crown body of this ball-crown body rotor arm is rotor mechanism protection cap, and described rotor mechanism protection cap is removably connected on ball-crown body rotor arm;Described body end face is provided with ball-crown body ceiling light;Described body bottom surface is provided with ball-crown body base;The bottom surface of described ball-crown body base is plane;The leading flank of described body is provided with photographic head and phonographic recorder, and the trailing flank of described body is provided with display screen, and the left and right side of described body is provided with loudspeaker;When unmanned plane is in folded state, four sides are surrounded by ball-crown body rotor arm entirely, make whole unmanned plane glomeration.
Due to said structure, being folded into by unmanned plane spherical, facilitate the storage of unmanned plane and carry, on unmanned plane, photographic head and the phonographic recorder of installing can be used in unmanned plane and carry out taking pictures, record a video, record, on unmanned plane, the ceiling light of installing potentially acts as desk lamp, for night illumination.On unmanned plane, the display screen of installing can be used in video recording and photo is play;Simultaneously because be equiped with loudspeaker on unmanned plane, this unmanned plane potentially acts as the audio amplifier of other outer audio equipments.
Further, described rotor mechanism includes bracing frame, micromachine and propeller;Support frame as described above is made up of 3 isometric support bars, and one end of every support bar intersects at a point, and forms Y-shaped in the same plane, and the angle between adjacent two bars is 120 °;The other end of every support bar is connected to ball-crown body rotor arm central circular cavity;Described micromachine is arranged on the point of intersection of support bar, and Miniature electric machine output shaft is straight up;On described Miniature electric machine output shaft, propeller is installed.
Further, described ball-crown body ceiling light includes ball-crown body transparent outer cover and the some LED covering in transparent outer cover;Described LED is arranged in array around the geometric center of end face.
The invention also discloses a kind of control system based on above-mentioned portable multi-function unmanned plane, described control system includes UAS and mobile terminal;Described UAS is arranged on internal body, described UAS includes unmanned plane main controller, described unmanned plane main controller connects and has power module, webcam driver module, video image memory module, phonographic recorder to drive module, recording memory module, button group, display screen to drive module, loudspeaker to drive module, LED to drive module, motor drive module;Wherein, webcam driver module is connected with photographic head, and described photographic head connects Computer Vision module, and this Computer Vision module is connected with video image memory module;Described recording drives module to be connected with phonographic recorder, and described phonographic recorder connects sound recording processing module, and this sound recording processing module is connected with recording memory module;Described motor drive module is connected with micromachine;Described LED drives module to be connected with LED;Described loudspeaker drive module to be connected with loudspeaker;Described display screen drives module to be connected with display screen;
Described button group includes the UAS start-stop button being arranged on base and LED start-stop button and is arranged on the video/audio control knob below display screen;Described video/audio control knob includes display screen start-stop button, video play button, picture playing button, volume knob;
Being also associated with wireless communication module on described unmanned plane main controller, unmanned plane main controller is connected with mobile terminal by wireless communication module;
The direction controlling module for controlling unmanned plane direction it is provided with, for controlling control module of taking pictures that photographic head takes pictures, for controlling video recording control module that the carrying out of photographic head and phonographic recorder record a video and for controlling the LED lamp control module of LED start and stop on described mobile terminal.
Further, described unmanned plane main controller is provided with external audio signal interface.
The invention also discloses a kind of control method based on above-mentioned portable multi-function unmanned plane, described control method includes, control method of taking photo by plane, LED control method and video/audio control method for playing back.
The step of described control method of taking photo by plane is as follows:
Step 1: all rotor arms are launched from folded state;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: send heading signal A to unmanned plane main controller by the direction controlling module on mobile terminal, unmanned plane main controller receives heading signal A and direction signal A is sent to motor drive module, make motor drive module control micromachine work, make unmanned plane towards different direction flight;
Step 4: adjust heading, adjust camera position, photographing signals is sent to unmanned plane main controller by the control module of taking pictures on mobile terminal, unmanned plane main controller receives photographing signals, and this photographing signals is sent to webcam driver module, make webcam driver module control minisize pick-up head work, make minisize pick-up head take pictures;The picture shot is stored in video image memory module after Computer Vision resume module;
Step 5: adjust heading, adjust camera position, video signal is sent to unmanned plane main controller by the video recording control module on mobile terminal, unmanned plane main controller receives video signal, and this video signal is sent to webcam driver module and phonographic recorder driving module, make webcam driver module control photographic head video recording and make phonographic recorder drive module control phonographic recorder to record;The video shot is stored in video image memory module after Computer Vision resume module;The recording recorded is stored in video image memory module after sound recording processing module processes;
Step 6: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal;
Step 7: all rotor arms are folded so that it is glomeration;
The step of described LED control method is as follows:
Step 1: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 2: send LED by the LED lamp control module on LED start-stop button or mobile terminal to unmanned plane main controller and light signal, unmanned plane main controller receive LED light signal and this LED is lighted signal be sent to LED drive module, make LED drive module control LED light.
Step 3: send LED black out signal to unmanned plane main controller by the LED lamp control module on LED start-stop button or mobile terminal, unmanned plane main controller receives LED and lights signal and this LED black out signal is sent to LED driving module, makes LED drive module to control LED and extinguishes.
Step 4: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal.
Video/audio control method for playing back:
Step 1: launched from folded state by rotor arm, exposes touch screen and audio amplifier;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: display screen start-stop button, sends display screen enabling signal, to unmanned plane main controller, unmanned plane main controller, display screen enabling signal is being sent to display screen driving module, be that display screen drives module to control display screen startup;
Step 4: press video play button, video display signals is sent to unmanned plane main controller, unmanned plane main controller receives this signal, and in video image memory module and recording storage, read video and recording respectively, then drive module to be sent to display screen display by display screen the video of reading and play;Drive evil spirit armour to be sent to loudspeaker by loudspeaker the recording of reading to play;
Step 5: press volume knob, sends volume adjustment signals to unmanned plane main controller, and unmanned plane main controller receives this signal and drives module to be sent to loudspeaker, and then regulation horn volume by loudspeaker this signal;
Step 6: press picture playing button, sends picture playing signal to unmanned plane main controller, and unmanned plane main controller receives this signal, reads picture, then drive module to be sent to display screen by display screen in the picture of reading and show in video image memory module;
Step 7: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal.
Step 8: all rotor arms are folded so that it is glomeration.
Further, described video/audio control method for playing back also includes external audio control method, and the step of this external audio control method is as follows:
Step 1: outer audio equipment is connected with unmanned plane main controller by external audio signal interface;
Step 2: outer audio equipment sends external audio signal by external audio signal interface to unmanned plane main controller, unmanned plane main controller receives this external audio signal, and drive module to be sent to loudspeaker by loudspeaker this external audio signal, make loudspeaker play this audio signal.
In sum, owing to have employed technique scheme, the invention has the beneficial effects as follows:
The portable multi-function unmanned plane volume of the present invention is little, it is simple to carry, and the unmanned plane application of the present invention is wide, it is possible to meet demand of taking photo by plane, it is possible to serve as desk lamp, carry out night illumination, it is possible to play video and picture, it is possible to as the audio amplifier of outer audio equipment.The present invention is practical, it is simple to promote.
Accompanying drawing explanation
Fig. 1 is the folded state diagram of the present invention;
Fig. 2 is the front view of the present invention;
Fig. 3 is deployed condition top view of the present invention;
Fig. 4 is camera position figure of the present invention;
Fig. 5 is the loudspeaker location drawing of the present invention;
Fig. 6 is screen position figure of the present invention;
Fig. 7 is control system figure of the present invention.
Detailed description of the invention
Below in conjunction with the accompanying drawings, the present invention is described in detail.
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein, only in order to explain the present invention, is not intended to limit the present invention.
The invention discloses a kind of portable multi-function unmanned plane, he includes that body 1, described body 1 include end face, bottom surface and all around four sides, and upper end, described each side is hinged with a ball-crown body rotor arm 2;Being circular cavity in the middle part of this ball-crown body rotor arm 2, be provided with rotor mechanism in cavity, the top ball-crown body of this ball-crown body rotor arm 2 is rotor mechanism protection cap 3, and described rotor mechanism protection cap 3 is removably connected on ball-crown body rotor arm 2;Described body end face is provided with ball-crown body ceiling light 4;Described body bottom surface is provided with ball-crown body base 5;The bottom surface of described ball-crown body base 5 is plane;The leading flank of described body is provided with photographic head 6 and phonographic recorder 7, and the trailing flank of described body is provided with display screen 8, and the left and right side of described body is provided with loudspeaker 9;When unmanned plane is in folded state, four sides are surrounded by ball-crown body rotor arm entirely, make whole unmanned plane glomeration.When unmanned plane is in state of flight, rotor arm protection cap thereon needs to pull down, it is to avoid hinder flight, when unmanned plane needs to store and carry is, can be by protection cap, in order to protection rotor mechanism.
Described rotor mechanism includes bracing frame, micromachine and propeller 11;Support frame as described above is made up of 3 isometric support bars 10, and one end of every support bar 10 intersects at a point, and forms Y-shaped in the same plane, and the angle between adjacent two bars is 120 °;The other end of every support bar 10 is connected to ball-crown body rotor arm 2 central circular cavity;Described micromachine is arranged on the point of intersection of support bar 10, and Miniature electric machine output shaft is straight up;Propeller 11 is installed on described Miniature electric machine output shaft.
Further, described ball-crown body ceiling light 4 includes ball-crown body transparent outer cover and the some LED covering in transparent outer cover;Described LED is arranged in array around the geometric center of end face.Wherein LED can fill class arrangement, polygonal array, meter Zi Hang arrangement, tetragon arrangement etc. ringwise.
The invention also discloses a kind of control system based on above-mentioned portable multi-function unmanned plane, described control system includes UAS and mobile terminal;Described UAS is arranged on internal body, described UAS includes unmanned plane main controller, described unmanned plane main controller connects and has power module, webcam driver module, video image memory module, phonographic recorder to drive module, recording memory module, button group, display screen to drive module, loudspeaker to drive module, LED to drive module, motor drive module;Wherein, webcam driver module is connected with photographic head, and described photographic head connects Computer Vision module, and this Computer Vision module is connected with video image memory module;Described recording drives module to be connected with phonographic recorder, and described phonographic recorder connects sound recording processing module, and this sound recording processing module is connected with recording memory module;Described motor drive module is connected with micromachine;Described LED drives module to be connected with LED;Described loudspeaker drive module to be connected with loudspeaker;Described display screen drives module to be connected with display screen;
Described button group includes the UAS start-stop button being arranged on base and LED start-stop button and is arranged on the video/audio control knob below display screen;Described video/audio control knob includes display screen start-stop button, video play button, picture playing button, volume knob;
Being also associated with wireless communication module on described unmanned plane main controller, unmanned plane main controller is connected with mobile terminal by wireless communication module;Described mobile terminal is mobile phone.
The direction controlling module for controlling unmanned plane direction it is provided with, for controlling control module of taking pictures that photographic head takes pictures, for controlling video recording control module that the carrying out of photographic head and phonographic recorder record a video and for controlling the LED lamp control module of LED start and stop on described mobile terminal.
Described unmanned plane main controller is provided with external audio signal interface.This interface is used for connecting outer audio equipment, so that unmanned plane uses as the audio amplifier of outer audio equipment.
The invention also discloses a kind of control method based on above-mentioned portable multi-function unmanned plane, described control method includes, control method of taking photo by plane, LED control method and video/audio control method for playing back.
The step of described control method of taking photo by plane is as follows:
Step 1: all rotor arms are launched from folded state;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: send heading signal A to unmanned plane main controller by the direction controlling module on mobile terminal, unmanned plane main controller receives heading signal A and direction signal A is sent to motor drive module, make motor drive module control micromachine work, make unmanned plane towards different direction flight;
Step 4: adjust heading, adjust camera position, photographing signals is sent to unmanned plane main controller by the control module of taking pictures on mobile terminal, unmanned plane main controller receives photographing signals, and this photographing signals is sent to webcam driver module, make webcam driver module control minisize pick-up head work, make minisize pick-up head take pictures;The picture shot is stored in video image memory module after Computer Vision resume module;
Step 5: adjust heading, adjust camera position, video signal is sent to unmanned plane main controller by the video recording control module on mobile terminal, unmanned plane main controller receives video signal, and this video signal is sent to webcam driver module and phonographic recorder driving module, make webcam driver module control photographic head video recording and make phonographic recorder drive module control phonographic recorder to record;The video shot is stored in video image memory module after Computer Vision resume module;The recording recorded is stored in video image memory module after sound recording processing module processes;
Step 6: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal;
Step 7: all rotor arms are folded so that it is glomeration;
The step of described LED control method is as follows:
Step 1: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 2: send LED by the LED lamp control module on LED start-stop button or mobile terminal to unmanned plane main controller and light signal, unmanned plane main controller receive LED light signal and this LED is lighted signal be sent to LED drive module, make LED drive module control LED light.
Step 3: send LED black out signal to unmanned plane main controller by the LED lamp control module on LED start-stop button or mobile terminal, unmanned plane main controller receives LED and lights signal and this LED black out signal is sent to LED driving module, makes LED drive module to control LED and extinguishes.
Step 4: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal.
Video/audio control method for playing back:
Step 1: launched from folded state by rotor arm, exposes touch screen and audio amplifier;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: display screen start-stop button, sends display screen enabling signal, to unmanned plane main controller, unmanned plane main controller, display screen enabling signal is being sent to display screen driving module, be that display screen drives module to control display screen startup;
Step 4: press video play button, video display signals is sent to unmanned plane main controller, unmanned plane main controller receives this signal, and in video image memory module and recording storage, read video and recording respectively, then drive module to be sent to display screen display by display screen the video of reading and play;Drive evil spirit armour to be sent to loudspeaker by loudspeaker the recording of reading to play;
Step 5: press volume knob, sends volume adjustment signals to unmanned plane main controller, and unmanned plane main controller receives this signal and drives module to be sent to loudspeaker, and then regulation horn volume by loudspeaker this signal;
Step 6: press picture playing button, sends picture playing signal to unmanned plane main controller, and unmanned plane main controller receives this signal, reads picture, then drive module to be sent to display screen by display screen in the picture of reading and show in video image memory module;
Step 7: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal.
Step 8: all rotor arms are folded so that it is glomeration.
Described video/audio control method for playing back also includes external audio control method, and the step of this external audio control method is as follows:
Step 1: outer audio equipment is connected with unmanned plane main controller by external audio signal interface;
Step 2: outer audio equipment sends external audio signal by external audio signal interface to unmanned plane main controller, unmanned plane main controller receives this external audio signal, and drive module to be sent to loudspeaker by loudspeaker this external audio signal, make loudspeaker play this audio signal.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all any amendment, equivalent and improvement etc. made within the spirit and principles in the present invention, should be included within the scope of the present invention.

Claims (7)

1. a portable multi-function unmanned plane, is characterized in that, it includes that body, described body include end face, bottom surface and all around four sides, and upper end, described each side is hinged with a ball-crown body rotor arm;Being circular cavity in the middle part of this ball-crown body rotor arm, be provided with rotor mechanism in cavity, the top ball-crown body of this ball-crown body rotor arm is rotor mechanism protection cap, and described rotor mechanism protection cap is removably connected on ball-crown body rotor arm;Described body end face is provided with ball-crown body ceiling light;Described body bottom surface is provided with ball-crown body base;The bottom surface of described ball-crown body base is plane;The leading flank of described body is provided with photographic head and phonographic recorder, and the trailing flank of described body is provided with display screen, and the left and right side of described body is provided with loudspeaker;When unmanned plane is in folded state, four sides are surrounded by ball-crown body rotor arm entirely, make whole unmanned plane glomeration.
A kind of portable multi-function unmanned plane the most according to claim 1, is characterized in that, described rotor mechanism includes bracing frame, micromachine and propeller;Support frame as described above is made up of 3 isometric support bars, and one end of every support bar intersects at a point, and forms Y-shaped in the same plane, and the angle between adjacent two bars is 120 °;The other end of every support bar is connected to ball-crown body rotor arm central circular cavity;Described micromachine is arranged on the point of intersection of support bar, and Miniature electric machine output shaft is straight up;On described Miniature electric machine output shaft, propeller is installed.
A kind of portable multi-function unmanned plane the most according to claim 2, is characterized in that, described ball-crown body ceiling light includes ball-crown body transparent outer cover and the some LED covering in transparent outer cover;Described LED is arranged in array around the geometric center of end face.
4. a control system for a kind of portable multi-function unmanned planes based on one of the claims 1 to 3, is characterized in that, described control system includes UAS and mobile terminal;Described UAS is arranged on internal body, described UAS includes unmanned plane main controller, described unmanned plane main controller connects and has power module, webcam driver module, video image memory module, phonographic recorder to drive module, recording memory module, button group, display screen to drive module, loudspeaker to drive module, LED to drive module, motor drive module;Wherein, webcam driver module is connected with photographic head, and described photographic head connects Computer Vision module, and this Computer Vision module is connected with video image memory module;Described recording drives module to be connected with phonographic recorder, and described phonographic recorder connects sound recording processing module, and this sound recording processing module is connected with recording memory module;Described motor drive module is connected with micromachine;Described LED drives module to be connected with LED;Described loudspeaker drive module to be connected with loudspeaker;Described display screen drives module to be connected with display screen;
Described button group includes the UAS start-stop button being arranged on base and LED start-stop button and is arranged on the video/audio control knob below display screen;Described video/audio control knob includes display screen start-stop button, video play button, picture playing button, volume knob;
Being also associated with wireless communication module on described unmanned plane main controller, unmanned plane main controller is connected with mobile terminal by wireless communication module;
The direction controlling module for controlling unmanned plane direction it is provided with, for controlling control module of taking pictures that photographic head takes pictures, for controlling video recording control module that the carrying out of photographic head and phonographic recorder record a video and for controlling the LED lamp control module of LED start and stop on described mobile terminal.
The control system of a kind of portable multi-function unmanned plane the most according to claim 4, is characterized in that, described unmanned plane main controller is provided with external audio signal interface.
6. a control method for a kind of portable multi-function unmanned plane based on claim 5, is characterized in that, described control method includes, control method of taking photo by plane, LED control method and video/audio control method for playing back:
The step of described control method of taking photo by plane is as follows:
Step 1: all rotor arms are launched from folded state;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: send heading signal A to unmanned plane main controller by the direction controlling module on mobile terminal, unmanned plane main controller receives heading signal A and direction signal A is sent to motor drive module, make motor drive module control micromachine work, make unmanned plane towards different direction flight;
Step 4: adjust heading, adjust camera position, photographing signals is sent to unmanned plane main controller by the control module of taking pictures on mobile terminal, unmanned plane main controller receives photographing signals, and this photographing signals is sent to webcam driver module, make webcam driver module control minisize pick-up head work, make minisize pick-up head take pictures;The picture shot is stored in video image memory module after Computer Vision resume module;
Step 5: adjust heading, adjust camera position, video signal is sent to unmanned plane main controller by the video recording control module on mobile terminal, unmanned plane main controller receives video signal, and this video signal is sent to webcam driver module and phonographic recorder driving module, make webcam driver module control photographic head video recording and make phonographic recorder drive module control phonographic recorder to record;The video shot is stored in video image memory module after Computer Vision resume module;The recording recorded is stored in video image memory module after sound recording processing module processes;
Step 6: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal;
Step 7: all rotor arms are folded so that it is glomeration;
The step of described LED control method is as follows:
Step 1: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 2: send LED by the LED lamp control module on LED start-stop button or mobile terminal to unmanned plane main controller and light signal, unmanned plane main controller receive LED light signal and this LED is lighted signal be sent to LED drive module, make LED drive module control LED light;
Step 3: send LED black out signal to unmanned plane main controller by the LED lamp control module on LED start-stop button or mobile terminal, unmanned plane main controller receives LED and lights signal and this LED black out signal is sent to LED driving module, makes LED drive module to control LED and extinguishes;
Step 4: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal;
Video/audio control method for playing back:
Step 1: launched from folded state by rotor arm, exposes touch screen and audio amplifier;
Step 2: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module connect with unmanned plane main controller, makes unmanned plane main controller in running order;
Step 3: display screen start-stop button, sends display screen enabling signal, to unmanned plane main controller, unmanned plane main controller, display screen enabling signal is being sent to display screen driving module, be that display screen drives module to control display screen startup;
Step 4: press video play button, video display signals is sent to unmanned plane main controller, unmanned plane main controller receives this signal, and in video image memory module and recording storage, read video and recording respectively, then drive module to be sent to display screen display by display screen the video of reading and play;Drive evil spirit armour to be sent to loudspeaker by loudspeaker the recording of reading to play;
Step 5: press volume knob, sends volume adjustment signals to unmanned plane main controller, and unmanned plane main controller receives this signal and drives module to be sent to loudspeaker, and then regulation horn volume by loudspeaker this signal;
Step 6: press picture playing button, sends picture playing signal to unmanned plane main controller, and unmanned plane main controller receives this signal, reads picture, then drive module to be sent to display screen by display screen in the picture of reading and show in video image memory module;
Step 7: press UAS start-stop button, transmission enabling signal, to UAS main controller, makes power module disconnect with unmanned plane main controller, allows unmanned plane main controller be in stopped status, and now UAS cannot receive any signal;
Step 8: all rotor arms are folded so that it is glomeration.
The control method of a kind of portable multi-function unmanned plane the most according to claim 6, is characterized in that, described video/audio control method for playing back also includes external audio control method, and the step of this external audio control method is as follows:
Step 1: outer audio equipment is connected with unmanned plane main controller by external audio signal interface;
Step 2: outer audio equipment sends external audio signal by external audio signal interface to unmanned plane main controller, unmanned plane main controller receives this external audio signal, and drive module to be sent to loudspeaker by loudspeaker this external audio signal, make loudspeaker play this audio signal.
CN201610376546.6A 2016-05-31 2016-05-31 portable multifunctional unmanned aerial vehicle Active CN105912023B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610376546.6A CN105912023B (en) 2016-05-31 2016-05-31 portable multifunctional unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610376546.6A CN105912023B (en) 2016-05-31 2016-05-31 portable multifunctional unmanned aerial vehicle

Publications (2)

Publication Number Publication Date
CN105912023A true CN105912023A (en) 2016-08-31
CN105912023B CN105912023B (en) 2019-12-13

Family

ID=56742930

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610376546.6A Active CN105912023B (en) 2016-05-31 2016-05-31 portable multifunctional unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN105912023B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109451238A (en) * 2017-11-23 2019-03-08 北京臻迪科技股份有限公司 A kind of communication means, communication system and unmanned plane

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201367115Y (en) * 2008-11-17 2009-12-23 西安智澜科技发展有限公司 Foldable four-axis multi-rotor wing aerocraft
CN202717030U (en) * 2012-07-25 2013-02-06 上海工程技术大学 Eight-axis rotor craft
US20150321755A1 (en) * 2014-04-28 2015-11-12 Arch Aerial, Llc Collapsible multi-rotor uav
CN204904034U (en) * 2015-09-02 2015-12-23 杨珊珊 Urgent medical rescue system and first -aid centre and first aid unmanned aerial vehicle thereof
CN205022843U (en) * 2015-08-04 2016-02-10 中国船舶工业系统工程研究院 Unmanned aerial vehicle organism is automatic to expand and folding mechanism
CN205098485U (en) * 2015-11-06 2016-03-23 刘东昌 Collapsible modularization unmanned aerial vehicle protection architecture
CN105460206A (en) * 2014-09-10 2016-04-06 深圳一电航空技术有限公司 Unmanned aerial vehicle
CN205880669U (en) * 2016-05-31 2017-01-11 王翔 Portable multi -functional unmanned aerial vehicle and control system thereof

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201367115Y (en) * 2008-11-17 2009-12-23 西安智澜科技发展有限公司 Foldable four-axis multi-rotor wing aerocraft
CN202717030U (en) * 2012-07-25 2013-02-06 上海工程技术大学 Eight-axis rotor craft
US20150321755A1 (en) * 2014-04-28 2015-11-12 Arch Aerial, Llc Collapsible multi-rotor uav
CN105460206A (en) * 2014-09-10 2016-04-06 深圳一电航空技术有限公司 Unmanned aerial vehicle
CN205022843U (en) * 2015-08-04 2016-02-10 中国船舶工业系统工程研究院 Unmanned aerial vehicle organism is automatic to expand and folding mechanism
CN204904034U (en) * 2015-09-02 2015-12-23 杨珊珊 Urgent medical rescue system and first -aid centre and first aid unmanned aerial vehicle thereof
CN205098485U (en) * 2015-11-06 2016-03-23 刘东昌 Collapsible modularization unmanned aerial vehicle protection architecture
CN205880669U (en) * 2016-05-31 2017-01-11 王翔 Portable multi -functional unmanned aerial vehicle and control system thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
极智: "团成一团翻滚吧!韩国厂商球形可折叠无人机", 《WWW.SOHU.COM/A/76037979_325474》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109451238A (en) * 2017-11-23 2019-03-08 北京臻迪科技股份有限公司 A kind of communication means, communication system and unmanned plane

Also Published As

Publication number Publication date
CN105912023B (en) 2019-12-13

Similar Documents

Publication Publication Date Title
EP4016984A1 (en) Optical image stabilization module and electronic device
CN102668536A (en) Control device, control method, image-capturing device, program, and image-capturing system
CN105163022B (en) Camera module and electronic device
CN105100311A (en) Mobile terminal
CN209545633U (en) Image runner assembly and electronic equipment
WO2019015118A1 (en) Image capturing apparatus, movable platform and image capturing device
CN106357981A (en) Shooting system
CN105912023A (en) Portable multifunctional unmanned aerial vehicle and control system and control method thereof
CN205880669U (en) Portable multi -functional unmanned aerial vehicle and control system thereof
KR20200000104A (en) Autonomous photographing apparatus
CN206002839U (en) A kind of panorama camera
US20120268569A1 (en) Composite camera system
CN206413076U (en) Wired flight camera
CN218243671U (en) Base and image acquisition device
CN110691181A (en) Camera equipment, cameras and drones
US12342058B2 (en) Multi-camera imaging device and system with simultaneous image/video capture
US11496654B2 (en) Projection-type video conference device and system there of
CN214397282U (en) Shooting device, cloud platform subassembly, many rotor unmanned aerial vehicle and unmanned aerial vehicle external member
JP2002359763A (en) Stand for digital camera
CN118450229B (en) Camera device and electronic equipment
WO2022141329A1 (en) Photographing device, control device, remote control device, mobile control system, and wearable device
CN206977581U (en) A kind of wireless session device
CN221058350U (en) A projection device
WO2020250249A1 (en) Apparatus and method for flying of a mobile device
CN112615996B (en) Dual-mode camera system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right
TA01 Transfer of patent application right

Effective date of registration: 20191106

Address after: 211302 ancient sandalwood Avenue, Gaochun District Economic Development Zone, Nanjing, Jiangsu Province, No. 3

Applicant after: Nanjing Hepu Aviation Technology Co., Ltd.

Address before: Wuhou District gold Yanlu Chengdu city in Sichuan province 610041 288 2 unit 5 Building No. 2

Applicant before: Wang Xiang

GR01 Patent grant
GR01 Patent grant