Automatic navigation flight control system based on cross-flow fan
A flight control system and automatic navigation technology, applied in the field of signal detection, can solve the problems of low cost, resistance to external force disturbance, controllability cannot meet actual requirements, and it is difficult to achieve the accuracy and reliability of professional inertial guidance units.
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[0040] The present invention will be further described below in conjunction with accompanying drawing.
[0041] Such as figure 1 As shown, this embodiment includes a power supply module, a microprocessor module, a fuselage attitude control module, a flying height detection module, a digital compass module, a wireless data transceiver module, a GPS positioning and navigation module, a serial port / SWD debugging interface circuit and signal input / Output Interface.
[0042] The specific work process of the present invention is: the body attitude control module, the flight height detection module real-time acquisition of data such as angular velocity, inclination acceleration and flight height of the three axes of the fuselage are sent to the microprocessor through the serial bus, and these data will be used as the main The flight inertial feedback information; the digital compass and GPS positioning navigation module collects the flight position feedback information such as head...
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