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Four-rotor aircraft control system based on dual-tone multi-frequency signal and method

A quad-rotor aircraft, dual-tone multi-frequency technology, applied in three-dimensional position/channel control, telephone communication, electrical components and other directions, can solve the problems of poor universality, limited control distance of quad-rotor aircraft, etc. The effect of limited control distance and extended control distance

Inactive Publication Date: 2012-11-28
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problems of limited control distance and poor universality of existing quadrotor aircraft, and propose a quadrotor aircraft control system and method based on dual-tone multi-frequency signal technology, which can realize real-time control of quadrotor aircraft , remote control, with strong universality

Method used

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  • Four-rotor aircraft control system based on dual-tone multi-frequency signal and method
  • Four-rotor aircraft control system based on dual-tone multi-frequency signal and method
  • Four-rotor aircraft control system based on dual-tone multi-frequency signal and method

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Embodiment

[0031] A quadrotor aircraft control system based on dual-tone multi-frequency signal technology, such as figure 1 As shown, it includes a DTMF signal receiving module 1 , a DTMF signal decoding module 5 , a main control module 6 , a flight control module 11 , a power supply module 15 and a user control terminal 18 .

[0032] Wherein, the DTMF signal receiving module 1 includes a GSM module 3, an audio interface 4 and a first serial interface 2, and a SIM card is installed in the GSM module 3. Wherein, the first serial interface 2 is used to set up the communication connection between the DTMF signal receiving module 1 and the main control module 6; the GSM module 3 receives the DTMF sent by the user control terminal 18 signal, and send the DTMF signal to the DTMF signal decoding module 5 through the audio interface 4.

[0033] In particular, for this control system, the GSM module 3 requires an AT command set that can be used to establish a connection with the main control m...

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Abstract

The invention provides a four-rotor aircraft control system based on a dual-tone multi-frequency signal and a method. The four-rotor aircraft control system comprises a dual-tone multi-frequency signal receiving module 1, a dual-tone multi-frequency signal decoding module 5, a main control module 6, a flying control module 11, a power supply module 12 and a user control terminal 18. A number corresponding to a subscriber identity module (SIM) card which is installed on the dual-tone multi-frequency signal receiving module 1 is dialed by a controller. A corresponding key is selected and touched by the controller according to the requirement after the connection, a dual-tone multi-frequency signal corresponding to the key is transmitted to the dual-tone multi-frequency signal receiving module 1, and finally the signal is transmitted to the dual-tone multi-frequency signal decoding module 5 to be decoded. A corresponding binary code is generated through the decoding, the main control module 6 reads the binary code to be solved so as to generate a corresponding pulse position modulation signal, the flying control module 11 obtains the voltage control quantity of a motor through the calculation according to the pulse position modulation signal so as to control the flying posture. Due to the adoption of the control system and the method, a telephone of any model can be connected with a four-rotor aircraft, so that the adaptability is strong, and the control distance is remarkably enlarged.

Description

technical field [0001] The invention relates to a control system and method for a quadrotor aircraft, in particular to a control system and method for a quadrotor aircraft based on dual-tone multi-frequency signals, and belongs to the technical fields of communication, signal processing and automatic control. Background technique [0002] With the rapid development of science and technology and the continuous improvement of people's living standards, remote-controlled aerial vehicles have greatly facilitated and enriched people's daily production and life, and are increasingly favored by people. Among them, the quadrotor aircraft is an aircraft with four propellers, and the four propellers are in a cross-shaped cross structure. The opposite quadrotors have the same rotation direction and are divided into two groups, and the rotation directions of the two groups are different (the four propellers can be Divided into two groups according to the direction of rotation, one posit...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10H04M11/02
Inventor 张婷程思源舒骏逸陈建良常彦春
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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