The invention discloses the measurement and
control system of a quad-rotor unmanned aerial vehicle scientific research and teaching
test bench. The
system is formed by a hardware circuit and measurement and
control software. The hardware circuit is formed by an angle
encoder, a main control
chip, a decoding board, a
gyroscope, a sensor, a remote controller, and an attitude adjustment mechanism. Anunmanned aerial vehicle rolling
signal is transmitted to
rolling angle control software via the angle
encoder and the decoding board, and an attitude response curve is displayed and a corresponding PID parameter is adjusted according to a curve change trend. The
software is used to feed back a parameter modification instruction to the main control
chip, and simultaneously, the desired posture ofa
remote control instruction is compared with the real-time posture monitored by the
gyroscope, and a result is used as a control input. Through the main control
chip, two input instructions are operated and processed, and then a corresponding control command is output. Through the organic combination of the
software and hardware, the smooth flight of the
single degree of freedom of an unmanned aerial vehicle is realized. The
system has guiding significance for studying the control mechanism of a rotor unmanned aerial vehicle, and has an important reference value for the development of an unmanned aerial
vehicle control system.