A semi-autonomous ground imitation flight system and control method for unmanned aerial vehicles
A control method and flight controller technology, applied in control/regulation systems, non-electric variable control, three-dimensional position/course control, etc., can solve problems such as unstable altitude control, barometer data interference, and susceptibility to interference, and achieve The effect of convenient operation
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[0024] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
[0025] A semi-autonomous ground imitation flight system for unmanned aerial vehicles, such as figure 1 As shown, it includes GPS positioning module, inertial measurement module, barometer module, radar altimeter, motor driver, propeller power structure and flight controller,
[0026] The GPS positioning module is connected to the flight controller through the UART interface, the inertial measurement module is connected to the flight controller through the SPI interface, the radar altimeter is connected to the flight controller through the UART interface, and the motor driver is connected to the flight controller through the PWM interface. The output shaft is connected to the power structure of the propeller, and the flight controller obtains the data of the GPS positioning module, the inertial measurement module and the radar altimeter to calculate the ...
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