CN211906054U - Integrated type flight release controller - Google Patents
Integrated type flight release controller Download PDFInfo
- Publication number
- CN211906054U CN211906054U CN202021054947.8U CN202021054947U CN211906054U CN 211906054 U CN211906054 U CN 211906054U CN 202021054947 U CN202021054947 U CN 202021054947U CN 211906054 U CN211906054 U CN 211906054U
- Authority
- CN
- China
- Prior art keywords
- controller
- throwing
- chip microcomputer
- single chip
- flying
- 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.)
- Active
Links
Images
Landscapes
- Toys (AREA)
Abstract
The utility model provides an integrated type flight input controller. The key points are as follows: it includes flies accuse ware and puts in controller, characterized by: the throwing controller is a single chip microcomputer, and the flying controller and the single chip microcomputer realize communication through TTL level signals, namely the TTL level connects the flying controller and the single chip microcomputer through three shielding wires TX, RX and GND; the flying controller and the throwing controller are installed in a mounting box, and an external interface of the flying controller and an external interface of the throwing controller are exposed out of the mounting box. The expected effect is: enabling the operation of the dispenser to share the resource of the flight controller; the flight controller and the throwing controller are integrated together, and the structure is compact.
Description
Technical Field
The utility model relates to an agricultural unmanned aerial vehicle's controller specifically is put in red eye bee ball unmanned aerial vehicle's integrated type flight control ware (henceforth called flight control ware) and puts in ware.
Background
CN209420481U discloses a dispenser for two-side dispensing trichogramma honeycomb (hereinafter referred to as bee ball), which is hung under an unmanned plane 5 and is suitable for being carried by and used in cooperation with the unmanned plane. This dispenser includes casing 201, screw drive axle 202, puts in mouth 2011, step motor 3 and power control system, and unmanned aerial vehicle directly supplies power for power control system and step motor, and step motor drive screw drive axle 202 is rotatory, and screw drive axle 202 drive honeycomb is put in to putting in mouth 2011. The unmanned aerial vehicle throwing device and the unmanned aerial vehicle share one power supply, and a power supply control system and a stepping motor are adopted as a control and power system, so that the accurate control capability is provided, and the throwing accuracy is improved (see 0028 and 0039 paragraphs of the specification). Obviously, the power control system is used as a launch controller, is independent of a flight controller (hereinafter referred to as a flight controller) of the unmanned aerial vehicle, and is respectively installed on the launch controller and the unmanned aerial vehicle. Because there is no communication between the throwing controller and the flying controller, the operation of the throwing device can not share the resource of the flying controller, namely, intelligent throwing of the trichogramma can not be realized.
Disclosure of Invention
In order to solve the technical problem, the utility model aims at providing an integrated type flight input controller.
The purpose of the utility model is realized like this: it includes flies accuse ware and puts in controller, characterized by: the throwing controller is a single chip microcomputer, and the flying controller and the single chip microcomputer realize communication through TTL level signals, namely the TTL level connects the flying controller and the single chip microcomputer through three shielding wires TX, RX and GND; the flying controller and the throwing controller are installed in a mounting box, and the external interface of the flying controller and the external interface of the throwing controller are exposed in the mounting box and are used for being connected with external equipment of the flying controller and the throwing controller respectively.
Will the utility model discloses install on unmanned aerial vehicle (the position of flying the accuse ware of original installation) or on the dispenser. The throwing controller is connected with external equipment, specifically, a positive pulse P + input end of a stepping motor driver of the throwing device is connected with a digital output pin of the single chip microcomputer, and a negative pulse P-input end is connected with a ground GND output pin of the single chip microcomputer. Wireless communication is realized between the flight controller and the ground controller through ZigBee.
The flight controller is the core for controlling the release, and is responsible for receiving GPS signals, communicating with the ground controller, controlling the flight of the unmanned aerial vehicle and communicating with the release controller. And (4) throwing the bee balls at fixed points by reading GPS signals in real time according to throwing interval time specified by a program and throwing coordinates set by calculation. When the singlechip program receives an instruction sent by the flight controller, the driver and the stepping motor of the throwing device are controlled to move once, and a bee ball is thrown.
Compared with the prior art, the utility model has the positive effects that: because the communication connection between the throwing controller and the flight controller is realized, the operation of the throwing device can share the resource of the flight controller, and the intelligent throwing of the trichogramma balls is realized; the flight controller and the throwing controller are integrated together, and the structure is compact.
Drawings
The present invention will be further described with reference to the accompanying drawings.
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is an electrical schematic diagram of the present invention.
Detailed Description
The ware of puting in of trichogrammatid honeycomb is put in to two sides is hung in unmanned aerial vehicle's below clearly, and unmanned aerial vehicle includes the flight control ware. The dispenser comprises a shell, a dispensing port, a dispensing controller, a stepping motor, a driver of the stepping motor and a laser counter; the laser counter is arranged at the throwing port of the shell, comprises a laser emitting end and a laser receiving end, is respectively arranged at the corresponding ends of the throwing channel of the throwing port and is positioned on the same straight line; referring to fig. 1, the launch controller is an arduino3.0nano single chip microcomputer, the flight controller 2 and the launch controller 3 are installed in a mounting box, the mounting box is composed of a box cover 1 and a box body 4, the external interface of the flight controller and the external interface of the launch controller are exposed in the mounting box, the mounting box comprises four vertical walls, two adjacent vertical walls 5 and 6 are respectively provided with a window (hole) 51 and 61, the external interface of the flight controller corresponds to the window 61, and the external interface of the launch controller corresponds to the window 51. Referring to fig. 2, the flight controller and the single chip microcomputer communicate with each other through a TTL level signal, that is, the TTL level connects the flight controller and the single chip microcomputer through three shielding wires (TX, RX, GND); connecting the throwing controller with external equipment, specifically connecting a laser emitting end with a power supply of a single chip microcomputer, and connecting a laser receiving end with a digital output pin of the single chip microcomputer; the positive pulse (P +) input end of the stepping motor driver is connected with a digital output pin of the singlechip, and the negative pulse (P-) input end is connected with a Ground (GND) output pin of the singlechip. Wireless communication is realized between the flight controller and the ground controller through ZigBee.
The working process is as described above.
Claims (2)
1. The utility model provides an integrated type flight input controller, it includes flies accuse ware and input controller, characterized by: the throwing controller is a single chip microcomputer, and the flying controller and the single chip microcomputer realize communication through TTL level signals, namely the TTL level connects the flying controller and the single chip microcomputer through three shielding wires TX, RX and GND; the flying controller and the throwing controller are installed in a mounting box, and an external interface of the flying controller and an external interface of the throwing controller are exposed out of the mounting box.
2. The integrated flight launch controller according to claim 1, wherein: the single chip microcomputer is a 3.0NANO single chip microcomputer; the external interface of the throwing controller is exposed in the mounting box, that is, the mounting box comprises four vertical walls, two adjacent vertical walls and a window are respectively arranged on the vertical walls, the external interface of the flight controller corresponds to one window, and the external interface of the throwing controller corresponds to the other window.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021054947.8U CN211906054U (en) | 2020-06-10 | 2020-06-10 | Integrated type flight release controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021054947.8U CN211906054U (en) | 2020-06-10 | 2020-06-10 | Integrated type flight release controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211906054U true CN211906054U (en) | 2020-11-10 |
Family
ID=73265987
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021054947.8U Active CN211906054U (en) | 2020-06-10 | 2020-06-10 | Integrated type flight release controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211906054U (en) |
-
2020
- 2020-06-10 CN CN202021054947.8U patent/CN211906054U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206594657U (en) | The serial transceiver controllers of multichannel UART based on bus communication | |
| CN206515700U (en) | A kind of UAV Flight Control System based on smart mobile phone | |
| CN108845587A (en) | Unmanned plane real-time control system and unmanned plane | |
| CN109726155A (en) | A kind of multi-bus interface system of airborne answering machine | |
| CN211906054U (en) | Integrated type flight release controller | |
| CN105711849A (en) | Unmanned aerial vehicle and flying state indicating method and device thereof | |
| CN211869699U (en) | Intelligent unmanned plane for putting trichogrammatid | |
| CN106789501A (en) | The bus control system and method for a kind of tandem type unmanned plane dynamical system | |
| CN207473414U (en) | A kind of unmanned aerial vehicle data communication control device | |
| CN201449530U (en) | Digital steering engine controller | |
| CN208459852U (en) | A kind of unmanned aerial vehicle control system | |
| CN205510322U (en) | Device based on optical ethernet interface transfer serial ports data | |
| CN111708374A (en) | Distributed power unmanned aerial vehicle control system | |
| CN207518852U (en) | Unmanned plane megaphone | |
| CN103349839B (en) | Safety control method of model airplane flight status | |
| CN102419586A (en) | Method for monitoring condition of unmanned aerial vehicle based on serial bus | |
| CN205983105U (en) | Unmanned aerial vehicle machine carries device management system | |
| CN211417591U (en) | Unmanned aerial vehicle of propaganda directed to communicate and propaganda directed to communicate carrying device thereof | |
| CN207799469U (en) | A kind of UAV Flight Control System based on ARM-M3 core chips | |
| CN202068371U (en) | Integrated two-phase step motor driver | |
| CN106032165B (en) | A kind of flying robot's foot structure | |
| CN210534586U (en) | Flight controller of fixed-wing unmanned aerial vehicle | |
| CN209674871U (en) | The circuit of unmanned plane Acoustic control remote controller | |
| CN208705727U (en) | Patrolling transmission line unmanned plane avoidance obstacle device | |
| CN108919700A (en) | For the data switching apparatus and unmanned plane in unmanned plane location navigation circuit |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210118 Address after: 3-3-3, no.39-3, Liaoshen Second Street, Dadong District, Shenyang City, Liaoning Province Patentee after: Cheng Guangyuan Patentee after: Cheng Dongmei Address before: 112600 2-3-1, 142 tianhougong Road, Dadong District, Shenyang City, Liaoning Province Patentee before: Wang Zhenyun |