CN204462856U - Portable unmanned machine manipulation case - Google Patents
Portable unmanned machine manipulation case Download PDFInfo
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- CN204462856U CN204462856U CN201520208930.6U CN201520208930U CN204462856U CN 204462856 U CN204462856 U CN 204462856U CN 201520208930 U CN201520208930 U CN 201520208930U CN 204462856 U CN204462856 U CN 204462856U
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Abstract
The utility model discloses a kind of Portable unmanned machine manipulation case, comprise casing and power supply, in casing, be provided with lower panel and top panel, in casing, be provided with Wireless Image Transmission Systems, wireless data communication system and wireless control system; Wireless Image Transmission Systems comprises wireless image transmission module, display screen and video antenna; Wireless data communication system comprises data transmission antenna, wireless data communication module and wireless signal transmitting module; Wireless control system comprises control signal antenna, sender unit and input equipment; Input equipment comprises height and direction controlling module.Beneficial effect is: unmanned plane and third party device can be made to communicate to connect, and makes operator's Real-Time Monitoring Unmanned Aerial Vehicle Data, strengthens the processing safety of unmanned plane; Flight course planning can be carried out to unmanned plane simultaneously, control simple, the manipulation of unmanned plane can be simplified, make ordinary person within several days, just can learn to handle, can control when unmanned plane exceeds visual line of sight.
Description
Technical field
The utility model relates to a kind of unmanned plane actuation means, particularly a kind of Portable unmanned machine manipulation case.
Background technology
At present, the manipulation of existing unmanned plane generally uses traditional double rocking lever telepilot to handle, operator is needed to make the aircraft that detects by an unaided eye during manipulation, the just uncontrollable unmanned plane when flying distance exceeds visual line of sight, and operator needs the manipulation of the training of a few year exercise ability skilled control double rocking lever and coordinates, significantly limit the quantity of unmanned plane operator, so that domestic unmanned plane specialty operator is very not enough, makes domestic unmanned air vehicle technique can not obtain sufficient development.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of Portable unmanned machine manipulation case, this manipulation case controls simple, the manipulation of unmanned plane can be simplified, make ordinary person within several days, just can learn to handle, can control when unmanned plane exceeds visual line of sight, and the data in unmanned plane during flying can be monitored.
For the utility model that solves the problem adopts following technical scheme:
A kind of Portable unmanned machine manipulation case, comprise by lower house and the hinged casing of upper shell and power supply, in lower house and upper shell, be respectively equipped with lower panel and top panel, in casing, be provided with Wireless Image Transmission Systems, wireless data communication system and wireless control system;
Described Wireless Image Transmission Systems comprises wireless image transmission module, display screen and video antenna on plate located in the above, video antenna, wireless image transmission module are connected by data line successively with display screen, for gathering and showing unmanned aerial vehicle onboard image in real time;
Described wireless data communication system comprises data transmission antenna, wireless data communication module and wireless signal transmitting module on plate located in the above, data transmission antenna, wireless data communication module are connected by data line successively with wireless signal transmitting module, for receiving the data of unmanned aerial vehicle onboard sensor and setting up WIFI LAN (Local Area Network), unmanned plane and third party device are communicated to connect by WIFI LAN (Local Area Network), and then makes operator by the flying quality of third party device Real-Time Monitoring unmanned plane and flight course planning is carried out to unmanned plane;
Described wireless control system comprises control signal antenna on plate located in the above, be located at sender unit on lower panel and input equipment, and the input end of sender unit is connected with input equipment and control signal antenna respectively with output terminal;
Described input equipment comprises:
Height control module, is arranged on lower panel, for controlling the flying height of unmanned plane;
Direction controlling module, is arranged on lower panel, for controlling the heading of unmanned plane.
As preferred further, described wireless image transmission module is wireless image transmission receiver, and wireless image transmission receiver is connected with the display control board of display screen by data line.
As preferred further, described video antenna is external high-gain rotary antenna.
As preferred further, described data transmission antenna is external high-gain rotary antenna.
As preferred further, described wireless data communication module is 900MHz data radio station.
As preferred further, described wireless signal transmitting module is WIFI signal transmitter.
As preferred further, be provided with rectangular notch in top panel side, described wireless image transmission module is connected with video output interface by data line, and video output interface is drawn by rectangular notch side, for placing third party device and connecting remote data indicator.
As further preferably, described sender unit comprises mainboard, be located at processor on mainboard and transmitter, and sender unit is connected with input equipment by mainboard, use wire to be connected by transmitter and control signal antenna.
As preferred further, described height control module is Slidable potentiometer, and the centre position of Slidable potentiometer is for controlling reference point, and controlling signals collecting information when being in this position is zero elevation change.
As preferred further, described direction controlling module is three axle rocker regulation resistances, for controlling the direction all around of unmanned plane.
As further preferably, described input equipment also comprises fine setting module, and it is arranged on lower panel, for the vernier control of the height and direction that realize unmanned plane.
As preferred further, described fine setting module adopts touch-switch, comprise height fine adjusting function button, front and back fine setting button, left and right fine setting button and directional trim button, front and back fine setting button, left and right fine setting button and directional trim button are arranged on around direction controlling module.
As preferred further, described sender unit is also furnished with regulating and controlling display screen and regulating and controlling button, for regulating the burden control of different unmanned plane.
As preferred further, described power supply to be located in lower house and to electrically connect respectively by wire and Wireless Image Transmission Systems, wireless data communication system and wireless control system, be connected to images/data power switch respectively at power output end and control power switch, for controlling the power switch of Wireless Image Transmission Systems, wireless data communication system and wireless control system.
As preferred further, on the mainboard of described sender unit, an input end is connected with RS232 interface, and described direction controlling module passes through RS232 interface and sender unit grafting, for realizing the detachable of direction controlling module.
As preferred further, in lower house, lower right-hand corner is provided with module standing groove, and described direction controlling module is detachably positioned in module standing groove, so that carry.
The beneficial effects of the utility model are:
1, the data of unmanned aerial vehicle onboard sensor can be received by the data transmission antenna of wireless data communication system and wireless data communication module and set up WIFI LAN (Local Area Network), unmanned plane and third party device (as computer, mobile phone, flat board etc.) are communicated to connect by WIFI LAN (Local Area Network), and then make operator by the various flying qualities of third party device Real-Time Monitoring unmanned plane, enhance the processing safety of unmanned plane; Can realize carrying out flight course planning to unmanned plane by the third party device of networking simultaneously, after on-course passing, manual operation is taken off, and open airline operation pattern, unmanned plane just can fly according to the course line of planning in advance automatically, without the need to hand control, conventional flight pattern will be changed.
2, can be used for respectively controlling the flying height of unmanned plane and heading by height control module and direction controlling module, greatly reduce the operating difficulty of unmanned plane operator, make ordinary person just can grasp method of operating within very short time, simultaneously can by unmanned aerial vehicle onboard picture showing on a display screen by Wireless Image Transmission Systems, operator still can be allowed to continue to handle even if make unmanned plane exceed visual line of sight, considerably increase the distance handled of unmanned plane, enhance the range of application of unmanned plane.
3, Wireless Image Transmission Systems, wireless data communication system and wireless control system are integrated in a casing, decrease the number of devices entrained by unmanned plane operator, effectively reduce the operating difficulty of unmanned plane.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural representation of upper shell in Fig. 1.
Fig. 3 is the structural representation of lower house in Fig. 1.
Fig. 4 is the rear view of top panel in Fig. 2.
Fig. 5 is the rear view of lower panel in Fig. 3.
Fig. 6 is the structural representation that the utility model casing removes upper and lower panel.
In figure: lower house 1, module standing groove 101, rectangular recess 102, rectangular slot 103, upper shell 2, top panel 3, lower panel 4, display screen 5, data transmission antenna 6, video antenna 7, control signal antenna 8, video output interface 9, rectangular notch 10, USB charging socket 11, wire perforation 12, wireless signal transmission lamp 13, data transfer signal lamp 14, pitch regulation module 15, control of sideward roll module 16, power supply upper cover 17, images/data power switch 18, control power switch 19, regulating and controlling display screen 20, menu enters button 21, on turn over button 22, under turn over button 23, exit button 24, increase button 25, reduce button 26, airline operation mode selection switch 27, throttle unlock switch 28, offline mode switch 29, directional trim button 30, direction controlling module 31, lock-screw 32, left and right fine setting button 33, front and back fine setting button 34, height fine adjusting function button 35, height control module 36, wireless image transmission module 37, control antenna mount pad 38, video antenna mount pad 39, data antenna mount pad 40, display control board 41, wireless data communication module 42, wireless signal transmitting module 43, transmitter 44, processor 45, mainboard 46, RS232 interface 47, power supply 48, installation frame 49.
Embodiment
As shown in figures 1 to 6, a kind of Portable unmanned machine manipulation case that the utility model relates to, comprise by lower house 1 and the hinged casing of upper shell 2, in lower house 1 and upper shell 2, cementation has installation frame 49 respectively, lower panel 4 and top panel 3 is respectively equipped with in lower house 1 and upper shell 2, lower panel 4 and top panel 3 are separately fixed on installation frame 49, are provided with Wireless Image Transmission Systems, wireless data communication system and wireless control system in casing.
As shown in Figure 2 and Figure 4, described Wireless Image Transmission Systems comprises wireless image transmission module 37, display screen 5 and video antenna 7 on plate 3 located in the above, video antenna 7, wireless image transmission module 37 are connected by data line successively with display screen 5, for gathering and showing unmanned aerial vehicle onboard image in real time.Described video antenna 7 is preferably external high-gain rotary antenna and is removably connected by screw thread and is arranged on a video antenna mount pad 39, described video antenna mount pad 39 is fixed in the above the upper center of plate 3 inside surface, top panel 3 is passed in its one end, for installing described video antenna 7.Described wireless image transmission module 37 is wireless image transmission receiver, and the output terminal of wireless image transmission receiver is connected with the display control board 41 after display screen 5 by data line.Described display screen 5 is preferably high definition TFT LCDs and the left upper portion of plate located in the above 3.
As preferred further, rectangular notch 10 is provided with on the right side of top panel 3, the output terminal of described wireless image transmission module 37 is connected with video output interface 9 by data line, video output interface 9 is drawn out in rectangular notch 10 by the installation frame 49 of rectangular notch 10 side, for placing third party device and connecting remote data indicator.USB charging socket 11 is provided with, for being described third party device charging in rectangular notch 10 side.
As shown in Figure 2 and Figure 4, described wireless data communication system comprises the data transmission antenna 6 on plate 3 located in the above, wireless data communication module 42 and wireless signal transmitting module 43, data transmission antenna 6, wireless data communication module 42 is connected by data line successively with wireless signal transmitting module 43, for receiving the data of unmanned aerial vehicle onboard sensor and setting up WIFI LAN (Local Area Network), unmanned plane and third party device are communicated to connect by WIFI LAN (Local Area Network), and then make operator by the flying quality of third party device Real-Time Monitoring unmanned plane and flight course planning is carried out to unmanned plane.
Described data transmission antenna 6 is preferably external high-gain rotary antenna and is removably connected by screw thread and is arranged on data antenna mount pad 40, data antenna mount pad 40 be fixed in the above plate 3 inside surface upper end on the left of and one end passed by top panel 3, for connecting described data transmission antenna 6.As preferably, described wireless data communication module 42 is 900MHz data radio station, and described wireless signal transmitting module 43 is WIFI signal transmitter.Wireless data communication module 42 and wireless signal transmitting module 43 are separately fixed at the inside surface of top panel 3 and are positioned at below display screen 5, wireless data communication module 42 is provided with data transfer signal lamp 14, wireless signal transmitting module 43 is provided with wireless signal transmission lamp 13, on described top panel 3, corresponding data signal transmission lamp 14 and wireless signal transmission lamp 13 place are respectively equipped with through hole, so that observe.
As Figure 2-Figure 5, described wireless control system comprises control signal antenna 8 on plate 3 located in the above, be located at sender unit on lower panel 4 and input equipment, and the input end of sender unit is connected with input equipment and control signal antenna 8 respectively with output terminal.As preferably, described sender unit is fixed on the lower surface upper right quarter of lower panel 4, it comprises mainboard 46, be arranged on processor 45 on mainboard 46 and transmitter 44, and the data after processor 45 processes are sent to transmitter 44 by the integrated circuit on mainboard 46.Sender unit is connected with each input equipment by the multiple input port on mainboard 46, is used wire to be connected by transmitter 44 with control signal antenna 8.Described control signal antenna 8 is preferably external high-gain rotary antenna and is detachably connected on a control antenna mount pad 38 by screw thread, described transmitter 44 is connected by wire with control antenna mount pad 38, described control antenna mount pad 38 be fixed in the above plate 3 inside surface upper end on the right side of and one end passed by top panel 3, for connecting described control signal antenna 8.Described transmitter 44 is preferably 2.4GHz transmitter.
As shown in Figure 3 and Figure 5, described input equipment comprises and is arranged on height control module 36 on lower panel 4 and direction controlling module 31, is respectively used to control flying height and all around direction of unmanned plane.Described height control module 36 is preferably Slidable potentiometer, it is arranged on the middle part of lower panel 4 inside surface, on top panel 3, the slide block place of corresponding Slidable potentiometer is provided with bar hole and described slide block is passed by bar hole, the centre position of Slidable potentiometer is for controlling reference point, and controlling signals collecting information when being in this position is zero elevation change.The right side that lower house 1 is positioned at height control module 36 is provided with a rectangular slot 103, a RS232 interface 47 is provided with in the bottom of rectangular slot 103, this RS232 interface 47 is connected with an input end on described mainboard 46 by wire, described direction controlling module 31 is three axle rocker regulation resistances and is inserted in rectangular slot 103, three axle rocker regulation resistances pass through plug and the grafting of described RS232 interface 47 of bottom, for realizing the detachable of direction controlling module 31.Below plate 4 is positioned at rectangular slot 103 both sides and is respectively equipped with lock-screw 32, for realize three axle rocker regulation resistances insert after spacing.In lower house 1, lower right-hand corner is provided with module standing groove 101, and described three axle rocker regulation resistances are detachably positioned in module standing groove 101, so that carry.Lower house 1 is positioned at lower panel 4 lower end and is provided with rectangular recess 102, for placing postrotational video antenna 7, data transmission antenna 6 and control signal antenna 8.
As preferably, described input equipment also comprises fine setting module and camera control module, wherein finely tunes the inside surface that module is fixed on lower panel 4, for the vernier control of the height and direction that realize unmanned plane.Described fine setting module adopts touch-switch, comprise height fine adjusting function button 35, front and back fine setting button 34, left and right fine setting button 33 and directional trim button 30, height fine adjusting function button 35 and front and back fine setting button 34 are arranged on the left side of three axle rocker regulation resistances, and directional trim button 30 and left and right fine setting button 33 are separately positioned on above and below three axle rocker regulation resistances.On plate 4, the button place of corresponding each fine setting button is respectively equipped with through hole below, for drawing each button.
As shown in Figure 3 and Figure 5, described camera control module comprises and is fixed on pitch regulation module 15 in the middle part of lower panel 4 and control of sideward roll module 16, described pitch regulation module 15 is Slidable potentiometer, for regulating the luffing angle of Airborne camera, control of sideward roll module 16 is rotating potentiometer, for regulating the left and right roll angle of Airborne camera.
As preferably, described sender unit is also furnished with regulating and controlling display screen 20 and regulating and controlling button, regulating and controlling display screen 20 is connected with the display translation end of processor 45, regulating and controlling button is connected respectively by the input end of wire with mainboard 46, for regulating the burden control of different unmanned plane and showing.Described regulating and controlling display screen 20 is arranged on the upper right quarter of lower panel 4, described regulating and controlling button comprises menu and enters button, on turn over button 22, under turn over button 23, exit button 24, increase button 25, reduce button 26, airline operation mode selection switch 27, throttle unlock switch 28 and offline mode switch 29, wherein menu enters button, on turn over button 22, under turn over button 23 and exit button 24, increase button 25, reduce button 26 and be arranged on both sides lower panel 4 being positioned at regulating and controlling display screen 20, airline operation mode selection switch 27, throttle unlock switch 28 and offline mode switch 29 are arranged on below lower panel 4 being positioned at regulating and controlling display screen 20.
As shown in Figure 6, power supply 48 is installed in the cavity on the left of lower house 1, be provided with power supply upper cover 17 power supply 48 cavity is suitable for reading, described power supply 48 is ferric phosphate lithium cell, power supply 48 electrically connects respectively by the modules of wire and Wireless Image Transmission Systems, wireless data communication system and wireless control system and display screen 5, be connected to images/data power switch 18 respectively at power supply 48 output terminal and control power switch 19 and USB charging socket 11, for controlling the power switch of Wireless Image Transmission Systems, wireless data communication system and wireless control system.Between top panel 3 with lower panel 4, being provided with corresponding wire mutually boring a hole 12, for running through power lead and data line.
Open casing, by each antenna manual rotation to upright position, three axle rocker regulation resistances are mounted in the rectangular slot 103 on the right side of lower panel 4, each switch is reset to initial position, the control slide block of height control module 36 is pulled down to minimum point, open and control power switch 19 and images/data power switch 18, the wait that switched on power by unmanned plane is subsequently taken off.
After taking off, the data of unmanned aerial vehicle onboard sensor can be received by data transmission antenna 6 and wireless data communication module 42 and set up WIFI LAN (Local Area Network), unmanned plane and third party device (as computer, mobile phone, flat board etc.) are communicated to connect by WIFI LAN (Local Area Network), and then makes operator by the various flying qualities of third party device Real-Time Monitoring unmanned plane.Can realize carrying out flight course planning to unmanned plane by the third party device of networking, after on-course passing, manual operation is taken off simultaneously, and open airline operation pattern, unmanned plane just can fly according to the course line of planning in advance automatically.Flying height and the heading of unmanned plane can be controlled by Slidable potentiometer, three axle rocker regulation resistances and fine setting module respectively, greatly reduce the operating difficulty of unmanned plane operator.When unmanned plane during flying exceeds visual line of sight, can by unmanned aerial vehicle onboard picture showing on display screen 5 by Wireless Image Transmission Systems, make operator still can continue to handle unmanned plane, considerably increase the distance handled of unmanned plane, enhance the range of application of unmanned plane.
When after the landing of control unmanned plane, unmanned plane power supply being disconnected, closing control power switch 19 and images/data power switch 18, being extracted to topple over by three axle rocker regulation resistances is positioned in the module standing groove 101 of lower panel 4, by each antenna manual rotation to horizontal level, closes casing.
Although embodiment of the present utility model is open as above, but it is not restricted to listed in instructions and embodiment utilization, it can be applied to various applicable field of the present utility model completely, for those skilled in the art, can easily realize other amendment, therefore do not deviating under the universal that claim and equivalency range limit, the utility model is not limited to specific details and illustrates here and the legend described.
Claims (10)
1. a Portable unmanned machine manipulation case, it is characterized in that: comprise by lower house and the hinged casing of upper shell and power supply, in lower house and upper shell, be respectively equipped with lower panel and top panel, in casing, be provided with Wireless Image Transmission Systems, wireless data communication system and wireless control system;
Described Wireless Image Transmission Systems comprises wireless image transmission module, display screen and video antenna on plate located in the above, video antenna, wireless image transmission module are connected by data line successively with display screen, for gathering and showing unmanned aerial vehicle onboard image in real time;
Described wireless data communication system comprises data transmission antenna, wireless data communication module and wireless signal transmitting module on plate located in the above, data transmission antenna, wireless data communication module are connected by data line successively with wireless signal transmitting module, for receiving the data of unmanned aerial vehicle onboard sensor and setting up WIFI LAN (Local Area Network), unmanned plane and third party device are communicated to connect by WIFI LAN (Local Area Network), and then makes operator by the flying quality of third party device Real-Time Monitoring unmanned plane and flight course planning is carried out to unmanned plane;
Described wireless control system comprises control signal antenna on plate located in the above, be located at sender unit on lower panel and input equipment, and the input end of sender unit is connected with input equipment and control signal antenna respectively with output terminal;
Described input equipment comprises:
Height control module, is arranged on lower panel, for controlling the flying height of unmanned plane;
Direction controlling module, is arranged on lower panel, for controlling the heading of unmanned plane.
2. Portable unmanned machine manipulation case according to claim 1, is characterized in that: described wireless image transmission module is wireless image transmission receiver, and wireless image transmission receiver is connected with the display control board of display screen by data line.
3. Portable unmanned machine manipulation case according to claim 1 and 2, is characterized in that: described video antenna is external high-gain rotary antenna.
4. Portable unmanned machine manipulation case according to claim 1, is characterized in that: described data transmission antenna is external high-gain rotary antenna.
5. the Portable unmanned machine manipulation case according to claim 1 or 4, is characterized in that: described wireless data communication module is 900MHz data radio station.
6. Portable unmanned machine manipulation case according to claim 5, is characterized in that: described wireless signal transmitting module is WIFI signal transmitter.
7. Portable unmanned machine manipulation case according to claim 1, it is characterized in that: be provided with rectangular notch in top panel side, described wireless image transmission module is connected with video output interface by data line, video output interface is drawn by rectangular notch side, for placing third party device and connecting remote data indicator.
8. Portable unmanned machine manipulation case according to claim 1, it is characterized in that: described sender unit comprises mainboard, be located at processor on mainboard and transmitter, and sender unit is connected with input equipment by mainboard, use wire to be connected by transmitter and control signal antenna.
9. the Portable unmanned machine manipulation case according to claim 1 or 8, it is characterized in that: described height control module is Slidable potentiometer, the centre position of Slidable potentiometer is for controlling reference point, and controlling signals collecting information when being in this position is zero elevation change.
10. Portable unmanned machine manipulation case according to claim 9, is characterized in that: described direction controlling module is three axle rocker regulation resistances, for controlling the direction all around of unmanned plane.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520208930.6U CN204462856U (en) | 2015-04-08 | 2015-04-08 | Portable unmanned machine manipulation case |
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| CN201520208930.6U CN204462856U (en) | 2015-04-08 | 2015-04-08 | Portable unmanned machine manipulation case |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104750114A (en) * | 2015-04-08 | 2015-07-01 | 王宏博 | Portable unmanned aerial vehicle control box |
| CN105388795A (en) * | 2015-12-18 | 2016-03-09 | 天津光电通信技术有限公司 | Miniaturized man-machine interaction system |
-
2015
- 2015-04-08 CN CN201520208930.6U patent/CN204462856U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104750114A (en) * | 2015-04-08 | 2015-07-01 | 王宏博 | Portable unmanned aerial vehicle control box |
| CN105388795A (en) * | 2015-12-18 | 2016-03-09 | 天津光电通信技术有限公司 | Miniaturized man-machine interaction system |
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| TR01 | Transfer of patent right |
Effective date of registration: 20190528 Address after: 121000 No. 164 Jiefang West Road, Taihe District, Jinzhou City, Liaoning Province Patentee after: Wang Quanchao Address before: No. 2-39, Baodi Manhattan, Songshan New District, Jinzhou City, Liaoning Province, 121000 Co-patentee before: Wang Quanchao Patentee before: Wang Hongbo |