CN109903540A - A model aircraft remote control system - Google Patents

A model aircraft remote control system Download PDF

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Publication number
CN109903540A
CN109903540A CN201711303904.1A CN201711303904A CN109903540A CN 109903540 A CN109903540 A CN 109903540A CN 201711303904 A CN201711303904 A CN 201711303904A CN 109903540 A CN109903540 A CN 109903540A
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China
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circuit
signal
frequency
encoder
frequency selection
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CN201711303904.1A
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路秀生
徐重阳
徐闯
刘世浩
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Northwest A&F University
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Northwest A&F University
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Priority to CN201711303904.1A priority Critical patent/CN109903540A/en
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Abstract

A kind of model airplane remote control system, belongs to remote control equipment field.Mainly it is made of crystal oscillator, high-frequency circuit, transmitting antenna, power supply, control stick, variable potentiometer, encoder, switching circuit, frequency selection circuit, receiving antenna, steering engine, decoding circuit and amplifying circuit, it is characterized by: control stick is connect with variable potentiometer, and variable potentiometer is connect with signal generator and encoder, signal caused by encoder is mounted on high-frequency circuit by switching circuit, frequency of oscillation is generated by crystal oscillator, is finally sent by transmitting transmitting antenna.Receiving antenna is connect with frequency selection circuit, frequency selection circuit is connected with crystal oscillator and amplifying circuit, and frequency selection circuit selects the signal to match and is transmitted to amplifying circuit, and amplifying circuit is connect with decoding circuit, signal is realized the conversion of signal by decoding circuit again after being amplified, decoding circuit is connect with steering engine again.

Description

一种航模遥控系统A model aircraft remote control system

技术领域technical field

本发明涉及一种航模遥控系统,属于遥控设备领域。The invention relates to a model aircraft remote control system, which belongs to the field of remote control equipment.

背景技术Background technique

航模遥控系统包括航模发射机和航模接收器,发射机是用来操控车模或船模的,由于它外部有一个长长的发射天线,遥控指令都是通过机壳外部的控制开关和按钮,经过内部电路的调制、编码,再通过高频信号放大电路由发射天线将电磁波发射出去。遥控接收机是安装在车模或船模上用来接收无线电信号的。它会处理来自遥控发射机的无线电信号,将所接收的信号进行放大、整形、解码,并把接收来的控制信号转换成执行电路可以识别的音频信号或是数字脉冲信号,传输给航模上的其他电子部件。但目前的航模遥控系统不稳定,因此迫切需要研发一种航模遥控系统。The model aircraft remote control system includes a model aircraft transmitter and a model aircraft receiver. The transmitter is used to control the car model or the ship model. Since it has a long transmitting antenna outside, the remote control commands are all through the control switches and buttons outside the casing. The modulation and coding of the internal circuit, and then the electromagnetic wave is emitted by the transmitting antenna through the high-frequency signal amplifying circuit. The remote control receiver is installed on the car model or ship model to receive radio signals. It processes the radio signal from the remote control transmitter, amplifies, shapes and decodes the received signal, and converts the received control signal into an audio signal or digital pulse signal that the executive circuit can recognize, and transmits it to the model aircraft. other electronic components. However, the current model aircraft remote control system is unstable, so there is an urgent need to develop a model aircraft remote control system.

发明内容SUMMARY OF THE INVENTION

针对上述不足,本发明提供了一种航模遥控系统。In view of the above deficiencies, the present invention provides a model aircraft remote control system.

本发明是通过以下技术方案实现的:一种航模遥控系统,是主要由晶体振荡器、高频电路、发射天线、电源、操纵杆、可变电位器、编码器、开关电路、选频电路、接收天线、舵机、译码电路和放大电路组成的,其特征在于:操纵杆与可变电位器连接,而可变电位器又与信号发生器和编码器连接,编码器所产生的信号通过开关电路搭载在高频电路上,由晶体振荡器产生振荡频率,最后由发射发射天线发送出去。接收天线与选频电路连接,选频电路与晶体振荡器和放大电路相连接,选频电路选出相匹配的信号传给放大电路,放大电路与译码电路连接,信号被放大后再由译码电路实现信号的转换,译码电路再与舵机连接。The invention is realized by the following technical solutions: a model aircraft remote control system mainly consists of a crystal oscillator, a high-frequency circuit, a transmitting antenna, a power supply, a joystick, a variable potentiometer, an encoder, a switch circuit, and a frequency selection circuit It is composed of a receiving antenna, a steering gear, a decoding circuit and an amplifying circuit. It is characterized in that the joystick is connected with the variable potentiometer, and the variable potentiometer is connected with the signal generator and the encoder. The signal is carried on the high-frequency circuit through the switch circuit, the oscillation frequency is generated by the crystal oscillator, and finally sent out by the transmitting and transmitting antenna. The receiving antenna is connected with the frequency selection circuit, the frequency selection circuit is connected with the crystal oscillator and the amplifier circuit, the frequency selection circuit selects the matching signal and transmits it to the amplifier circuit, the amplifier circuit is connected with the decoding circuit, and the signal is amplified and then converted by the decoding circuit. The code circuit realizes the conversion of the signal, and the decoding circuit is connected with the steering gear.

所述的编码器可以实现模拟信号到数字信号的转换。The encoder can realize the conversion of analog signal to digital signal.

所述的译码电路可以实现数字信号到模拟信号的转换。The decoding circuit can realize the conversion of digital signal to analog signal.

该发明的有益之处是:使操纵者的操作快速有效的通过发射机发射出去,实现精确控制,尽量减少了其他信号的干扰,而且可以准确的接收相匹配的信号,并使接收到的信号快速有效的传给舵机,实现精确控制,减少了其他信号的干扰。The advantages of the invention are: the operator's operation can be quickly and effectively transmitted through the transmitter to achieve precise control, minimize the interference of other signals, and can accurately receive the matching signal, and make the received signal It is quickly and effectively transmitted to the steering gear to achieve precise control and reduce the interference of other signals.

附图说明Description of drawings

图1为本发明发射机的系统结构图;图2为本发明接收器的系统结构图;Fig. 1 is the system structure diagram of the transmitter of the present invention; Fig. 2 is the system structure diagram of the receiver of the present invention;

图中,1、晶体振荡器,2、高频电路,3、发射天线,4、电源,5、操纵杆,6、可变电位器,7、编码器,8、开关电路,9、选频电路,10、接收天线,11、舵机,12、译码电路,13、放大电路。In the figure, 1. Crystal oscillator, 2. High frequency circuit, 3. Transmitting antenna, 4. Power supply, 5. Joystick, 6. Variable potentiometer, 7. Encoder, 8. Switch circuit, 9. Selection Frequency circuit, 10. Receiving antenna, 11. Steering gear, 12. Decoding circuit, 13. Amplifying circuit.

具体实施方式Detailed ways

一种航模遥控系统,是主要由晶体振荡器1、高频电路2、发射天线3、电源4、操纵杆5、可变电位器6、编码器7、开关电路8、选频电路9、接收天线10、舵机11、译码电路12和放大电路13组成的,其特征在于:操纵杆5与可变电位器6连接,而可变电位器6又与信号发生器和编码器7连接,编码器7所产生的信号通过开关电路8搭载在高频电路2上,由晶体振荡器1产生振荡频率,最后由发射天线3发送出去。接收天线10与选频电路9连接,选频电路9与晶体振荡器1和放大电路13相连接,选频电路9选出相匹配的信号传给放大电路13,放大电路13与译码电路12连接,信号被放大后再由译码电路12实现信号的转换,译码电路12再与舵机11连接。An aircraft model remote control system is mainly composed of a crystal oscillator 1, a high-frequency circuit 2, a transmitting antenna 3, a power supply 4, a joystick 5, a variable potentiometer 6, an encoder 7, a switch circuit 8, a frequency selection circuit 9, The receiving antenna 10, the steering gear 11, the decoding circuit 12 and the amplifying circuit 13 are composed, and it is characterized in that: the joystick 5 is connected with the variable potentiometer 6, and the variable potentiometer 6 is connected with the signal generator and the encoder. 7 is connected, the signal generated by the encoder 7 is carried on the high-frequency circuit 2 through the switch circuit 8, the oscillation frequency is generated by the crystal oscillator 1, and finally sent out by the transmitting antenna 3. The receiving antenna 10 is connected to the frequency selection circuit 9, the frequency selection circuit 9 is connected to the crystal oscillator 1 and the amplifier circuit 13, the frequency selection circuit 9 selects the matched signal and transmits it to the amplifier circuit 13, and the amplifier circuit 13 and the decoding circuit 12 After the signal is amplified, the signal is converted by the decoding circuit 12 , and the decoding circuit 12 is then connected to the steering gear 11 .

所述的编码器7可以实现模拟信号到数字信号的转换。The encoder 7 can realize the conversion of analog signals to digital signals.

所述的译码电路12可以实现数字信号到模拟信号的转换。The decoding circuit 12 can realize the conversion of digital signals to analog signals.

该装置在工作时,由操作人员操作操纵杆5,使可变电位器6电压发生变化,可变电位器6与信号发生电路连接,从而信号发生电路产生变化的电压信号,信号发生电路和编码器7连接,变化的电压信号经过编码器7转换成数字信号,编码器7产生的数字信号再通过开关电路8搭载在高频电路2上由发射天线3发送出去,实现信号的发射,从接收放大电路13出来的脉冲信号,通过译码电路12后就能分别独立地取出由发射机发出的操纵杆5动作信号,并分配到不同的译码地址输出口。When the device is working, the operator operates the joystick 5 to change the voltage of the variable potentiometer 6, and the variable potentiometer 6 is connected with the signal generating circuit, so that the signal generating circuit generates a changed voltage signal, and the signal generating circuit Connected with the encoder 7, the changed voltage signal is converted into a digital signal through the encoder 7, and the digital signal generated by the encoder 7 is then mounted on the high-frequency circuit 2 through the switch circuit 8 and sent out by the transmitting antenna 3 to realize the transmission of the signal, The pulse signal from the receiving amplifying circuit 13 can be independently extracted from the operating signal of the joystick 5 sent by the transmitter after passing through the decoding circuit 12, and distributed to different decoding address output ports.

对于本领域的普通技术人员而言,根据本发明的教导,在不脱离本发明的原理与精神的情况下,对实施方式所进行的改变、修改、替换和变型仍落入本发明的保护范围之内。For those of ordinary skill in the art, according to the teachings of the present invention, without departing from the principle and spirit of the present invention, changes, modifications, substitutions and alterations to the embodiments still fall within the protection scope of the present invention within.

Claims (3)

1.一种航模遥控系统,是主要由晶体振荡器、高频电路、发射天线、电源、操纵杆、可变电位器、编码器、开关电路、选频电路、接收天线、舵机、译码电路和放大电路组成的,其特征在于:操纵杆与可变电位器连接,而可变电位器又与信号发生器和编码器连接,编码器所产生的信号通过开关电路搭载在高频电路上,由晶体振荡器产生振荡频率,最后由发射发射天线发送出去。接收天线与选频电路连接,选频电路与晶体振荡器和放大电路相连接,选频电路选出相匹配的信号传给放大电路,放大电路与译码电路连接,信号被放大后再由译码电路实现信号的转换,译码电路再与舵机连接。1. A model aircraft remote control system is mainly composed of a crystal oscillator, a high-frequency circuit, a transmitting antenna, a power supply, a joystick, a variable potentiometer, an encoder, a switch circuit, a frequency selection circuit, a receiving antenna, a steering gear, a translation It is composed of a code circuit and an amplifier circuit, and is characterized in that: the joystick is connected with the variable potentiometer, and the variable potentiometer is connected with the signal generator and the encoder, and the signal generated by the encoder is carried on the high-speed switch circuit through the switch circuit. On the frequency circuit, the oscillation frequency is generated by the crystal oscillator, and finally sent out by the transmitting and transmitting antenna. The receiving antenna is connected with the frequency selection circuit, the frequency selection circuit is connected with the crystal oscillator and the amplifier circuit, the frequency selection circuit selects the matching signal and transmits it to the amplifier circuit, the amplifier circuit is connected with the decoding circuit, and the signal is amplified and then converted by the decoding circuit. The code circuit realizes the conversion of the signal, and the decoding circuit is connected with the steering gear. 2.如权利要求1所述的一种航模发射机系统,其特征在于:所述的编码器可以实现模拟信号到数字信号的转换。2. A model aircraft transmitter system according to claim 1, characterized in that: the encoder can realize the conversion of analog signal to digital signal. 3.如权利要求1所述的一种航模发射机系统,其特征在于:所述的译码电路可以实现数字信号到模拟信号的转换。3 . The model aircraft transmitter system according to claim 1 , wherein the decoding circuit can realize the conversion from digital signals to analog signals. 4 .
CN201711303904.1A 2017-12-11 2017-12-11 A model aircraft remote control system Pending CN109903540A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711303904.1A CN109903540A (en) 2017-12-11 2017-12-11 A model aircraft remote control system

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Application Number Priority Date Filing Date Title
CN201711303904.1A CN109903540A (en) 2017-12-11 2017-12-11 A model aircraft remote control system

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CN109903540A true CN109903540A (en) 2019-06-18

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021042725A1 (en) * 2019-09-04 2021-03-11 深圳市富斯科技有限公司 Unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021042725A1 (en) * 2019-09-04 2021-03-11 深圳市富斯科技有限公司 Unmanned aerial vehicle

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