CN203102009U - Four rotor aircraft control system based on mobile phone short messages - Google Patents

Four rotor aircraft control system based on mobile phone short messages Download PDF

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Publication number
CN203102009U
CN203102009U CN 201320029529 CN201320029529U CN203102009U CN 203102009 U CN203102009 U CN 203102009U CN 201320029529 CN201320029529 CN 201320029529 CN 201320029529 U CN201320029529 U CN 201320029529U CN 203102009 U CN203102009 U CN 203102009U
Authority
CN
China
Prior art keywords
module
input end
control system
rotor aircraft
micro controller
Prior art date
Application number
CN 201320029529
Other languages
Chinese (zh)
Inventor
姬江涛
贺智涛
侯鲁
郑治华
何亚凯
扈菲菲
杜新武
杜蒙蒙
金鑫
贾世通
邓明俐
Original Assignee
河南科技大学
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 河南科技大学 filed Critical 河南科技大学
Priority to CN 201320029529 priority Critical patent/CN203102009U/en
Application granted granted Critical
Publication of CN203102009U publication Critical patent/CN203102009U/en

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Abstract

The utility model belongs to the field of four rotor aircrafts, and in particular relates to a four rotor aircraft control system based on mobile phone short messages. The four rotor aircraft control system based on the mobile phone short messages comprises a GSM module, a micro controller, a flight control module, a propeller drive motor and a user short message platform. The user short message platform realizes communication with the GSM module of a four rotor aircraft by editing a short message. The output end of the GSM module is connected with the input end of the micro controller. The output end of the micro controller is connected with the input end of the flight control module. The output end of the flight control module is connected with the input end of the propeller drive motor. The control system is further provided with a GPS module. The data output end of the GPS module is connected with the input end of the micro controller. The control system is further provided with an earth magnetic position sensor. The data output end of the earth magnetic position sensor is connected with the input end of the micro controller. According to the utility model, the design is ingenious; various function controls can be remotely carried out on the four rotor aircraft; and the application prospect of the four rotor aircraft is expanded.

Description

A kind of four rotor craft control system based on SMS

Technical field

The utility model belongs to four rotor craft fields, is specifically related to a kind of four rotor craft control system based on SMS.

Background technology

Four rotor crafts are a kind of aircraft with four screw propellers, and four rotors are divided into two groups, and the sense of rotation of two groups of rotors is opposite.

Four rotor crafts must be realized various flare maneuvers by the speed that changes each screw propeller.

Four traditional rotor crafts generally adopt telepilot to control flare maneuver, but its remote control distance are limited, and must with the supporting use of aircraft.

After four rotor crafts are installed various scientific instrument, can be applicable to scientific research and other field, as field information acquisition, forest resourceies exploration, disaster relief etc., at this moment, the flying distance of four rotor crafts will can't realize the control to four rotor crafts considerably beyond effective remote control distance of telepilot.

At present, the someone proposes to adopt landline telephone or mobile phone to send touch-tone signal as control command, comes received signal by the touch-tone signal receiver module on four rotor crafts, realizes the far distance controlled to four rotor crafts.

But adopt touch-tone signal 16 kinds of control commands to be arranged at most, can not satisfy the multi-functional control of people four rotor crafts as control command.

In addition, adopt touch-tone signal as control command, receiver module need be set be responsible for receiving touch-tone signal, send decoder module then to, by decoder module the touch-tone signal of receiving is become binary code, as 0000,0001,0002 etc., send binary code to main control module then, decode procedure relies on hardware to finish, complex steps, the reaction velocity when influencing four rotor crafts reception control command.

The utility model content

The purpose of this utility model provides a kind of four rotor craft control system based on SMS, can not only realize the multiple function control to four rotor crafts, and system is simple, the reaction velocity when improving four rotor crafts reception control command greatly.

Technical solution adopted in the utility model is: a kind of four rotor craft control system based on SMS comprise gsm module, microcontroller, flight control module, screw propeller drive motor and user's SMS platform; Described user's SMS platform realizes communicating by letter with the gsm module of four rotor crafts by editing short message, the output terminal of gsm module links to each other with the input end of microcontroller, the output terminal of microcontroller links to each other with the input end of flight control module, and the output terminal of flight control module links to each other with the input end of screw propeller drive motor.

Described control system also is provided with the GPS module, and the data output end of GPS module is connected with the input end of microcontroller.

Described control system also is provided with the magnetic azimuth sensor, and the data output end of magnetic azimuth sensor is connected with the input end of microcontroller.

The beneficial effects of the utility model are: the utility model is by adopting short message content as control command, the note of editor's certain content, send to the gsm module on four rotor crafts, the different different control commands of short message content representative, the content of SMS can reach 140 characters at most, control command can define a variety of, has realized at a distance the multiple function of four rotor crafts being controlled; Receiving end of the present utility model comprises gsm module and microcontroller, disposal route is, receive the note that user's SMS platform sends by gsm module, content with note sends to microcontroller then, does not need decoder module, and microcontroller is according to the content of note, form different control commands, and control command sent to subsequent control equipment, this process is finished by the software in the microcontroller, has improved the reaction velocity when four rotor crafts receive control command greatly.

Description of drawings

Fig. 1 is a structural representation of the present utility model.

Mark among the figure: 1, user's SMS platform, 2, gsm module, 3, microcontroller, 4, the flight control module, 5, the screw propeller drive motor, 6, the GPS module, 7, the magnetic azimuth sensor.

Embodiment

Below in conjunction with the drawings and specific embodiments the utility model is elaborated, as shown in the figure: a kind of four rotor craft control system based on SMS comprise gsm module 2, microcontroller 3, flight control module 4, screw propeller drive motor 5 and user's SMS platform 1; Described user's SMS platform 1 realizes communicating by letter with the gsm module 2 of four rotor crafts by editing short message, the output terminal of gsm module 2 links to each other with the input end of microcontroller 3, the output terminal of microcontroller 3 links to each other with the input end of flight control module 4, and the output terminal of flight control module 4 links to each other with the input end of screw propeller drive motor 5.

Described control system also is provided with GPS module 6, and the data output end of GPS module 6 is connected with the input end of microcontroller 3.

Described control system also is provided with magnetic azimuth sensor 7, and the data output end of magnetic azimuth sensor 7 is connected with the input end of microcontroller 3.

Using method of the present utility model may further comprise the steps:

Step 1: short message content is set to instruction, and the corresponding relation of short message content and instruction is stored in the code of four rotor craft microcontrollers 3;

Step 2: the effector uses user's SMS platform 1 editing short message, send to the gsm module 2 of four rotor crafts, after gsm module 2 is received note, short message content is given microcontroller 3, microcontroller 3 is analyzed short breath contents, obtains user's steering order, and according to the data of GPS module 6 and magnetic azimuth sensor 7, generation is to the control command of flight control module 4, thereby controls the flare maneuver that four rotor crafts are finished appointment.

Claims (1)

1. four rotor craft control system based on SMS is characterized in that: comprise GPS module (6), magnetic azimuth sensor (7), gsm module (2), microcontroller (3), flight control module (4), screw propeller drive motor (5) and user's SMS platform (1); Described user's SMS platform (1) realizes communicating by letter with the gsm module (2) of four rotor crafts by editing short message, the output terminal of gsm module (2) links to each other with the input end of microcontroller (3), the output terminal of microcontroller (3) links to each other with the input end of flight control module (4), the output terminal of flight control module (4) links to each other with the input end of screw propeller drive motor (5), and the output terminal of GPS module (6) and magnetic azimuth sensor (7) links to each other with the input end of microcontroller (3) respectively.
CN 201320029529 2013-01-21 2013-01-21 Four rotor aircraft control system based on mobile phone short messages CN203102009U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320029529 CN203102009U (en) 2013-01-21 2013-01-21 Four rotor aircraft control system based on mobile phone short messages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320029529 CN203102009U (en) 2013-01-21 2013-01-21 Four rotor aircraft control system based on mobile phone short messages

Publications (1)

Publication Number Publication Date
CN203102009U true CN203102009U (en) 2013-07-31

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Family Applications (1)

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CN 201320029529 CN203102009U (en) 2013-01-21 2013-01-21 Four rotor aircraft control system based on mobile phone short messages

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CN (1) CN203102009U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103792947A (en) * 2014-02-28 2014-05-14 哈尔滨伟方智能科技开发有限责任公司 Small rotor flying robot for medical assistance
CN104133483A (en) * 2014-07-08 2014-11-05 遵义师范学院 Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof
CN104851275A (en) * 2015-05-18 2015-08-19 张金柱 Quadcopter combined with intelligent mobile phone
CN105589469A (en) * 2014-10-21 2016-05-18 武汉乐享视界科技有限公司 Quadcopter using Wi-Fi in manipulation and video transmission
CN105824320A (en) * 2016-04-25 2016-08-03 至简天蕴智控科技(苏州)有限公司 Aircraft emergency control device and control method thereof

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103792947A (en) * 2014-02-28 2014-05-14 哈尔滨伟方智能科技开发有限责任公司 Small rotor flying robot for medical assistance
CN104133483A (en) * 2014-07-08 2014-11-05 遵义师范学院 Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof
CN105589469A (en) * 2014-10-21 2016-05-18 武汉乐享视界科技有限公司 Quadcopter using Wi-Fi in manipulation and video transmission
CN104851275A (en) * 2015-05-18 2015-08-19 张金柱 Quadcopter combined with intelligent mobile phone
CN105824320A (en) * 2016-04-25 2016-08-03 至简天蕴智控科技(苏州)有限公司 Aircraft emergency control device and control method thereof

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GR01 Patent grant
C14 Grant of patent or utility model
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130731

Termination date: 20140121

C17 Cessation of patent right