CN104634386A - Intelligent aircraft system - Google Patents
Intelligent aircraft system Download PDFInfo
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- CN104634386A CN104634386A CN201410711393.7A CN201410711393A CN104634386A CN 104634386 A CN104634386 A CN 104634386A CN 201410711393 A CN201410711393 A CN 201410711393A CN 104634386 A CN104634386 A CN 104634386A
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Abstract
The invention discloses an intelligent aircraft system, and belongs to the field of wireless control. The intelligent aircraft system is characterized by comprising a GPS (global positioning system) module, an electronic compass, a distance measurement module, an electric drive, a wireless controller, data acquisition devices, a wireless module, a sensor, an accelerometer, a battery management module and a control terminal; the GPS module is connected with the wireless controller; the electronic compass, the distance measurement module, the control terminal, the battery management module, the sensor, the accelerometer and the wireless controller are connected with the data acquisition devices; the wireless module and the electric drive are connected with the wireless controller. The intelligent aircraft system has the advantages that data can be monitored and remotely controlled over long distances by the aid of wireless transmission, the diversified data acquisition devices and positioning devices of the intelligent control system, and accordingly the intelligent aircraft system is high in stability, simple in operation and suitable to be popularized and utilized in various fields and has perfect functions.
Description
Technical field
the invention belongs to controlled in wireless field, particularly relate to a kind of aircraft systems of intelligence.
Background technology
Along with the continuous progress of science and technology, increasing intelligent electronic device has entered into the life of people, brings great convenience to the life of people, and it is more and more wider that the application in every field relates to face.Along with the continuous appearance of energy crisis in recent years, people are sharply expanding for the exploitation of marine energy, just propose new higher requirement for the electronic intelligence sniffer adapted to; Simultaneously when the disaster such as earthquake, rubble flow occurs, for the temporary transient unapproachable high-risk area of personnel, the use of smart machine is with regard to necessity very, and also more and more higher to the requirement of intelligent system.Therefore, the monitoring platform developing the higher intelligence of a integrated level is needed.
Summary of the invention
The present invention is intended to solve the problem, and provides a kind of aircraft systems of intelligence.
An aircraft systems for intelligence, is characterized in that comprising GPS module, electronic compass, range finder module, motorized motions, wireless controller, data collector, wireless module, sensor, accelerometer, battery management module and control terminal; Wherein GPS module is connected with wireless controller; Electronic compass, range finder module, control terminal, battery management module, sensor, accelerometer are all connected with data collector with wireless controller; Wireless module is all connected with controlled in wireless with motorized motions.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described controller adopts DSPIC30F4011 singlechip chip.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described sensor comprises wind speed wind direction sensor, temperature sensor, humidity sensor and baroceptor.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described wind speed wind direction sensor is PH100SX sensor.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that the frequency of described wind speed wind direction sensor is 1kHz.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described temperature sensor is DS1820 digital temperature sensor.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described baroceptor is the integrated baroceptor of MS5561.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described humidity sensor is SYHS220 sensor.
The aircraft systems of a kind of intelligence of the present invention, is characterized in that described wireless module adopts RFC30F wireless communication module.
The aircraft systems of a kind of intelligence of the present invention, by the application of intelligent control system, in conjunction with several data harvester and locating device, wireless transmission is utilized to realize remote data monitoring and remote control, native system stability is high, simple to operate, perfect in shape and function, be adapted at multi-field in promote the use of.
Embodiment
An aircraft systems for intelligence, is characterized in that comprising GPS module, electronic compass, range finder module, motorized motions, wireless controller, data collector, wireless module, sensor, accelerometer, battery management module and control terminal; Wherein GPS module is connected with wireless controller; Electronic compass, range finder module, control terminal, battery management module, sensor, accelerometer are all connected with data collector with wireless controller; Wireless module is all connected with controlled in wireless with motorized motions.
The aircraft systems of a kind of intelligence of the present invention, described controller adopts DSPIC30F4011 singlechip chip, inner with DSP engine, data processing extensive, at a high speed can be carried out, and built-in A/D modular converter, spi bus module, CAN module, UART module etc., utilize these modules can the design of peripheral circuits, strengthen the reliability of system, shorten the construction cycle.Described sensor comprises wind speed wind direction sensor, temperature sensor, humidity sensor and baroceptor.Described wind speed wind direction sensor is PH100SX sensor.The frequency of described wind speed wind direction sensor is 1kHz, adopts the input capture of single-chip microcomputer to measure.When air velocity transducer frequency signal rising edge arrives, input capture will produce interruption, now write down the numerical value in timer, two numerical value write down by twice interruption are subtracted each other, simultaneously according to timer period, just can calculate the frequency values of wind velocity signal, calculate wind speed.The transducer of wind transducer adopts precision conductive plastic potentiometer, thus exports at the resistance signal that the movable end of potentiometer changes, and the A/D sample conversion through single-chip microcomputer is 10 position digital signals, then calculates wind direction value.The north point of determining of the positive dirction of the positive dirction of digital compass, intelligent platform, wind transducer is specified point-blank, revises wind direction by course angle, obtain actual wind direction numerical value, namely depart from the angle of geographic north.After protocol conversion, these wind speed, wind direction, acceleration and compass data gps data are sent in CAN.Described temperature sensor is DS1820 digital temperature sensor, provide the temperature of 9 temperature reading indicating devices, measurement range is from-55 ~+125 DEG C, and increment size is 0.5 DEG C.Described baroceptor is the integrated baroceptor of MS5561, it is a SMD hydrid integrated circuit being integrated with piezoresistive pressure sensor and ADC interface, 16 bit data word depending on pressure and temperature can be provided, communicate with microprocessor by 3 line serial line interfaces.。Described humidity sensor is SYHS220 sensor, and only need be connected with single-chip microcomputer by one-wire interface, then be changed by A/D, algorithm process can obtain humidity value.Described wireless module adopts RFC-30F wireless communication module, and RFC-30F monolithic wireless transceiver is operated in the ISM band of 433MHz.The parameter of surrounding environment by the structure of self poisoning and map, and is passed to by platform the information that long-range parametric controller obtains environment by some sensors by aircraft systems of the present invention, thus realizes monitoring and the information acquisition of data.
Claims (9)
1. an intelligent aircraft systems, is characterized in that comprising GPS module, electronic compass, range finder module, motorized motions, wireless controller, data collector, wireless module, sensor, accelerometer, battery management module and control terminal; Wherein GPS module is connected with wireless controller; Electronic compass, range finder module, control terminal, battery management module, sensor, accelerometer are all connected with data collector with wireless controller; Wireless module is all connected with controlled in wireless with motorized motions.
2. the aircraft systems of a kind of intelligence as claimed in claim 1, is characterized in that described controller adopts DSPIC30F4011 singlechip chip.
3. the aircraft systems of a kind of intelligence as claimed in claim 1, is characterized in that described sensor comprises wind speed wind direction sensor, temperature sensor, humidity sensor and baroceptor.
4. the aircraft systems of a kind of intelligence as claimed in claim 3, is characterized in that described wind speed wind direction sensor is PH100SX sensor.
5. the aircraft systems of a kind of intelligence as claimed in claim 4, is characterized in that the frequency of described wind speed wind direction sensor is 1kHz.
6. the aircraft systems of a kind of intelligence as claimed in claim 3, is characterized in that described temperature sensor is DS1820 digital temperature sensor.
7. the aircraft systems of a kind of intelligence as claimed in claim 3, is characterized in that described baroceptor is the integrated baroceptor of MS5561.
8. the aircraft systems of a kind of intelligence as claimed in claim 3, is characterized in that described humidity sensor is SYHS220 sensor.
9. the aircraft systems of a kind of intelligence as claimed in claim 1, is characterized in that described wireless module adopts RFC30F wireless communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410711393.7A CN104634386A (en) | 2014-12-01 | 2014-12-01 | Intelligent aircraft system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410711393.7A CN104634386A (en) | 2014-12-01 | 2014-12-01 | Intelligent aircraft system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104634386A true CN104634386A (en) | 2015-05-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410711393.7A Pending CN104634386A (en) | 2014-12-01 | 2014-12-01 | Intelligent aircraft system |
Country Status (1)
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| CN (1) | CN104634386A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105319218A (en) * | 2015-12-15 | 2016-02-10 | 广西师范大学 | Unmanned aerial vehicle building flaw detection system based on FPGA |
| CN106064098A (en) * | 2016-06-02 | 2016-11-02 | 镇江市高等专科学校 | A kind of mesoporous class graphitic carbon nitride/palladium composite material, Its Preparation Method And Use |
| CN109425914A (en) * | 2017-08-31 | 2019-03-05 | 广东泰高新技术发展有限公司 | Mobile weather station and the intelligent catapult-launching gear using the movement weather station |
| CN117268170A (en) * | 2023-10-23 | 2023-12-22 | 广州天海翔航空科技有限公司 | Unmanned aerial vehicle ejection control method, device, equipment and storage medium |
-
2014
- 2014-12-01 CN CN201410711393.7A patent/CN104634386A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105319218A (en) * | 2015-12-15 | 2016-02-10 | 广西师范大学 | Unmanned aerial vehicle building flaw detection system based on FPGA |
| CN106064098A (en) * | 2016-06-02 | 2016-11-02 | 镇江市高等专科学校 | A kind of mesoporous class graphitic carbon nitride/palladium composite material, Its Preparation Method And Use |
| CN109425914A (en) * | 2017-08-31 | 2019-03-05 | 广东泰高新技术发展有限公司 | Mobile weather station and the intelligent catapult-launching gear using the movement weather station |
| CN109425914B (en) * | 2017-08-31 | 2021-06-04 | 广东泰一高新技术发展有限公司 | Remove meteorological station and use this intelligence jettison device who removes meteorological station |
| CN117268170A (en) * | 2023-10-23 | 2023-12-22 | 广州天海翔航空科技有限公司 | Unmanned aerial vehicle ejection control method, device, equipment and storage medium |
| CN117268170B (en) * | 2023-10-23 | 2024-03-22 | 广州天海翔航空科技有限公司 | Unmanned aerial vehicle ejection control method, device, equipment and storage medium |
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Legal Events
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150520 |
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| WD01 | Invention patent application deemed withdrawn after publication |