CN205405267U - Six spool miniature aircraft - Google Patents
Six spool miniature aircraft Download PDFInfo
- Publication number
- CN205405267U CN205405267U CN201620163223.4U CN201620163223U CN205405267U CN 205405267 U CN205405267 U CN 205405267U CN 201620163223 U CN201620163223 U CN 201620163223U CN 205405267 U CN205405267 U CN 205405267U
- Authority
- CN
- China
- Prior art keywords
- miniature
- microcontroller
- module
- communication module
- adopts
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model discloses a six spool miniature aircraft, including the installation main part there are six spiral arms according to circumference evenly distributed in the installation main part, do not are provided with a motor in the tip punishment of being close to every spiral arm, at each be provided with the rotor in the pivot of motor the below of installation main part is provided with shuts down the frame, the installation main part is a circuit installation cavity, is provided with microcontroller among the control circuit of this circuit installation cavity inside, the motor that microcontroller controlled respectively on each spiral arm rotates last gyroscope sensor, acceleration sensor, magnetometer sensor, temperature sensor, status display module, gesture display module, power and the communication module of still being connected with of microcontroller. Beneficial effect: six spool miniature aircraft simple structure, easy control, flexible, control efficiency is high, and bearing capacity is good, and adaptability is strong, and the reaction is rapid, and the range of application is wide, and the accuracy is high.
Description
Technical field
This utility model relates to flying vehicles control technical field, specifically a kind of miniature six axle aircraft.
Background technology
Miniature six axle aircraft are unmanned vehicles, possess can the advantage such as vertical lift, freedom of the air hovering, all have broad application prospects at modern military and civilian convenience.Military affairs are applied to ground battle reconnaissance and the aspect such as supervision, explosive, information acquisition, closely aerial support；May be used on civilian taking photo by plane, search and rescue after natural disaster, high-voltage line, dam inspection etc..Therefore the research carrying out minute vehicle has very great meaning.
But owing to miniature six axle aircraft body sizes are little, it is bigger than normal to conduct oneself with dignity, flight speed is low, and its flight Reynolds number is relatively low, simultaneously, miniature six axle aircraft are also one and have 6, a space degree of freedom and the under-actuated systems of only 4 inputs, have the characteristics such as multivariate, non-linear and close coupling.Therefore, the miniature six portable equipment of axle aircraft and payload have been affected by great restriction, and its payload capability is little, it is difficult to efficiently accomplish complex task, makes the development of minute vehicle be extremely limited.
Utility model content
For the problems referred to above, this utility model provides a kind of miniature six axle aircraft, arranges microcontroller and various module on miniature six axle aircraft, increases the carrying energy of aircraft, adaptive capacity, response speed, expands range of application, makes degree of accuracy improve.
For reaching above-mentioned purpose, the concrete technical scheme that this utility model adopts is as follows:
A kind of miniature six axle aircraft, including mounting body, described mounting body there are six spiral arms according to even circumferential distribution, it is respectively arranged with a motor in the end near each spiral arm, at each described, the rotating shaft of motor is provided with rotor, described mounting body be arranged below shut down frame, described mounting body is a circuit installation cavity, this is provided with microcontroller in control circuit within circuit installation cavity, described microcontroller controls the electric machine rotation on each spiral arm respectively, it is also associated with gyro sensor on the microcontroller, acceleration transducer, magnetometer sensor, temperature sensor, state display module, attitude display module, power supply and communication module.
By above-mentioned design; the microprocessor controls motor of miniature six axle aircraft rotates according to default parameter; and in conjunction with gyro sensor, acceleration transducer, magnetometer sensor, the various parameters of temperature sensor detection and the parameter such as throttle, course, rolling, pitching; realize different state of flights; and shown by state display module, wherein state of flight include vertical ascent, vertically decline, be moved to the left, move right, move forward, be moved rearwards by, crabbing, hovering, emergency shutdown etc.；State display module includes that wireless telecommunications show, starting state shows, emergency shutdown is reported to the police, charging indicates, running status, charge condition, power supply instruction etc..
Further describe, in order to make microcontroller can be precisely controlled miniature six axle aircraft, and the data of each sensor can be read in time, carry out data quick-processing, control motor, related data passed to other miniature six axle aircraft by communication module and on miniature six axle aircraft, shows in real time the flight attitude of aircraft, microcontroller employing LPC2148 single-chip microcomputer；In order to make gyro sensors taken up space little, low in energy consumption, location is accurate, precision high, described gyro sensor adopts FXAS21002 tri-number of axle word rate-of-turn gyroscope；In order to reduce the weight of whole aircraft, making circuit more succinct, described acceleration transducer and magnetometer sensor adopt one piece of highly integrated chip, described acceleration transducer and magnetometer sensor to adopt FXOS8700CQ integration module；In order to improve the precision of measurement, described temperature sensor adopts model to be the digital temperature sensor of DS18B20；Described communication module includes ZigBee wireless communication module.
Further describe, control miniature six axle aircraft to realize ground, described microcontroller is also associated with WiFi wireless communication module and GPS locating module.
Preferably, described WiFi wireless communication module adopts RN1723, and described GPS locating module adopts BU-1315.
Further describe, in order to shoot the environment residing for miniature six axle aircraft, so that user controls miniature six axle aircraft in real time, described mounting body is provided with camera module, in order to preserve the various data of miniature six axle aircraft, facilitate customer analysis to check the log of miniature six axle aircraft, analyze the flight progress of miniature six axle aircraft, be connected to SD card memory module on the microcontroller.
Yet further, in order to make ZigBee wireless communication module have higher receiving sensitivity and interference free performance, described ZigBee wireless communication module adopts CC2530F64, and in order to improve shooting quality, described camera module adopts OV16825-2A.
The beneficial effects of the utility model: miniature six axle Flight Vehicle Structures are simple, it is easy to control, maneuverability, control efficiency is high, and bearing capacity is good, adaptable, is swift in response, applied range, and degree of accuracy is high.
Accompanying drawing explanation
Fig. 1 is the miniature six axle Flight Vehicle Structure schematic diagrams of this utility model；
Fig. 2 is the circuit structure block diagram of miniature six axle aircraft of the present utility model；
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model and operation principle are described in further detail.
Can be seen that from Fig. 1 and Fig. 2, a kind of miniature six axle aircraft, including mounting body, mounting body there are six spiral arms according to even circumferential distribution, it is respectively arranged with a motor in the end near each spiral arm, the rotating shaft of each motor is provided with rotor, mounting body be arranged below shut down frame, mounting body is a circuit installation cavity, this is provided with microcontroller in control circuit within circuit installation cavity, microcontroller controls the electric machine rotation on each spiral arm respectively, it is also associated with gyro sensor on a microcontroller, acceleration transducer, magnetometer sensor, temperature sensor, state display module, attitude display module, power supply and communication module.
Figure it is seen that in the present embodiment, the communication module connected on miniature six axle aircraft is ZigBee wireless communication module, and ZigBee wireless communication module adopts CC253F64.
Preferably, in the present embodiment, microcontroller adopts LPC2148 single-chip microcomputer；Gyro sensor adopts FXAS21002 tri-number of axle word rate-of-turn gyroscope；Acceleration transducer and magnetometer sensor adopt FXOS8700CQ integration module；Temperature sensor adopts model to be the digital temperature sensor of DS18B20；
Figure it is seen that be also associated with camera module and SD card memory module on the microcontroller of miniature six axle aircraft, it is preferable that camera module adopts OV16825-2A.
Claims (6)
1. miniature six axle aircraft, including mounting body, it is characterized in that, described mounting body there are six spiral arms according to even circumferential distribution, it is respectively arranged with a motor in the end near each spiral arm, at each described, the rotating shaft of motor is provided with rotor, described mounting body be arranged below shut down frame, described mounting body is a circuit installation cavity, this is provided with microcontroller in control circuit within circuit installation cavity, described microcontroller controls the electric machine rotation on each spiral arm respectively, it is also associated with gyro sensor on the microcontroller, acceleration transducer, magnetometer sensor, temperature sensor, state display module, attitude display module, power supply and communication module.
2. the miniature six axle aircraft of one according to claim 1, it is characterized in that, described microcontroller adopts LPC2148 single-chip microcomputer, described gyro sensor adopts FXAS21002 tri-number of axle word rate-of-turn gyroscope, described acceleration transducer and magnetometer sensor adopt FXOS8700CQ integration module, described temperature sensor adopts model to be the digital temperature sensor of DS18B20, and described communication module includes ZigBee wireless communication module.
3. the miniature six axle aircraft of one according to claim 2, it is characterised in that be also associated with WiFi wireless communication module and GPS locating module on the microcontroller.
4. miniature six axle aircraft according to claim 3, it is characterised in that described WiFi wireless communication module adopts RN1723, described GPS locating module adopts BU-1315.
5. according to the arbitrary described miniature six axle aircraft of one of claim 1-4, it is characterised in that be provided with camera module in described mounting body, be connected to SD card memory module on the microcontroller.
6. the miniature six axle aircraft of one according to claim 5, it is characterised in that described ZigBee wireless communication module adopts CC2530F64, described camera module adopts OV16825-2A.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620163223.4U CN205405267U (en) | 2016-03-03 | 2016-03-03 | Six spool miniature aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620163223.4U CN205405267U (en) | 2016-03-03 | 2016-03-03 | Six spool miniature aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205405267U true CN205405267U (en) | 2016-07-27 |
Family
ID=56443454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620163223.4U Expired - Fee Related CN205405267U (en) | 2016-03-03 | 2016-03-03 | Six spool miniature aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205405267U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105549609A (en) * | 2016-03-03 | 2016-05-04 | 四川理工学院 | Miniature six-shaft aircraft, air fleet control system composed of same and air fleet control method |
| CN109814470A (en) * | 2019-03-26 | 2019-05-28 | 河南小兵网络科技有限公司 | A kind of quadrotor drone monitoring comprehensive platform |
| US20210086907A1 (en) * | 2019-09-20 | 2021-03-25 | Bioniwings (Beijing) Technology Co. Ltd. | Aircraft, Control Method, Apparatus and Computer Readable Storage Medium for Aircraft |
-
2016
- 2016-03-03 CN CN201620163223.4U patent/CN205405267U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105549609A (en) * | 2016-03-03 | 2016-05-04 | 四川理工学院 | Miniature six-shaft aircraft, air fleet control system composed of same and air fleet control method |
| CN109814470A (en) * | 2019-03-26 | 2019-05-28 | 河南小兵网络科技有限公司 | A kind of quadrotor drone monitoring comprehensive platform |
| US20210086907A1 (en) * | 2019-09-20 | 2021-03-25 | Bioniwings (Beijing) Technology Co. Ltd. | Aircraft, Control Method, Apparatus and Computer Readable Storage Medium for Aircraft |
| US11577850B2 (en) * | 2019-09-20 | 2023-02-14 | Hanwang Technology Co., Ltd. | Aircraft, control method, apparatus and computer readable storage medium for aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205554560U (en) | Unmanned vehicles and frame thereof | |
| CN104149982B (en) | Air quality detector based on quadcopter | |
| CN102424112B (en) | Three-layer airborne flight control device for micro four-rotor aerial vehicle | |
| CN105539037A (en) | Land-air four-rotor-wing unmanned aerial vehicle capable of rolling on ground | |
| CN105334861A (en) | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane | |
| CN105607640B (en) | The Pose Control device of quadrotor | |
| CN205405267U (en) | Six spool miniature aircraft | |
| US11926414B2 (en) | Underwater and aerial vehicle | |
| CN105955305A (en) | Four-axis unmanned aerial vehicle | |
| CN106325289A (en) | Renesas R5F100LEA master control-based four-rotor flight controller and control method thereof | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN105549609A (en) | Miniature six-shaft aircraft, air fleet control system composed of same and air fleet control method | |
| CN205060006U (en) | Four -rotor unmanned aerial vehicle | |
| CN108910040A (en) | Mobile device aircraft | |
| CN205384514U (en) | Survey many rotor unmanned aerial vehicle flight control | |
| CN205594456U (en) | But voice warning keeps away four rotor unmanned vehicles of barrier | |
| CN109398686B (en) | Rotor unmanned aerial vehicle and attitude control method thereof | |
| CN110488857A (en) | A kind of control system of the quadrotor unmanned vehicle of solar energy | |
| CN205581550U (en) | Four miniature rotor unmanned aerial vehicle controlling means | |
| CN110398574B (en) | Water surface movable water quality monitoring node device based on raspberry pie | |
| CN107571990A (en) | A kind of highly sensitive three axles unmanned plane | |
| CN103019243B (en) | Based on the self-navigation aircraft of cross flow fan | |
| CN204489201U (en) | Based on the quadrotor flight system of STM32 | |
| CN202975811U (en) | Automatic navigation aircraft based on cross-flow fan | |
| CN207173952U (en) | A kind of rotor wing unmanned aerial vehicle and its control system for flying control plate based on APM |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160727 Termination date: 20200303 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |