A small fixed-wing unmanned aerial vehicle guidance computer and guidance method
A UAV, fixed-wing technology, applied in attitude control, control/regulation system, non-electric variable control, etc., to achieve the effect of improving design efficiency
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[0039] The invention will be described in further detail below in conjunction with the accompanying drawings.
[0040] 1. Guidance computer design
[0041] The guidance computer is the core of the guidance system. The whole system consists of two boards, namely the power supply board and the control signal processing board. The whole system consists of two boards, namely the power board and the control signal processing board. The power board includes a power conversion circuit module and an analog reference voltage module. The control signal processing board includes an IO driver module, an analog signal conditioning module, a digital signal conditioning module and a CPU module. High reliability and low power consumption.
[0042]a. The module used for the guidance computer DC / DC (direct current-direct current) conversion used in the present invention is LT3972, and the 27V input voltage is converted into +5V output, and the digital circuit work is provided; the 27V input ...
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