Minisize quadrotor-aircraft control system based on integrated positioning communication module and control method thereof

Abstract

The invention provides a minisize quadrotor-aircraft control system based on an integrated positioning communication module. The system includes an integrated positioning communication module, a central controller, a flying control module, a propeller driving motor, a three-shaft gyroscope, a power supply energy-saving module, a charging management module, a battery, a charging port and a geomagnetism orientation sensor. All of data output ends of the integrated positioning communication module, the three-shaft gyroscope, the power supply energy-saving module and the geomagnetism orientation sensor are connected with input ends of the central controller. An output end of the central controller is connected with an input end of the propeller driving motor via the flying control module. The minisize quadrotor-aircraft control system and the control method thereof adopt a method of GSM / GPS dual positioning method so that information and signal transmission can be carried out through wide utilization of internet or other mobile networks and the like and thus great convenience is brought to positioning and flying; effective energy distribution of the system complies with a modern concept of low carbon and environment protection and thus the system is low in cost, high in efficiency and energy saving.

Description

technical field [0001] The invention relates to a micro quadrotor aircraft control system and a control method based on an integrated positioning communication module. Background technique [0002] As early as the middle of the last century, micro-miniature multi-rotor aircraft have been favored by some overseas research institutions, but multi-rotor aircraft are generally small in size and poor in load capacity, and cannot be equipped with traditional high-precision sensors. Until the beginning of this century, the development of MEMS sensor technology made a breakthrough in the research of micro multi-rotor aircraft. [0003] The four propellers of the quadrotor aircraft are divided into two groups, and the rotation directions are opposite. Various flight actions must be completed by changing the speed of each propeller. After installing various scientific instruments, the traditional quadrotor aircraft can be used in scientific research and other fields, such as the coll...

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Problems solved by technology

[0004] In order to solve the above technical problems, the present invention provides a micro quadrotor control system and its control method based on the integrated positioning communication module. Module, central controller, flight control module, propeller drive motor, three-axis gyroscope, power saving module, etc. solve the problems of heavy weight, limited communication distance and poor real-time effect of the aircraft itself

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