Unmanned aerial vehicle integrated computer, computer-based control system and computer-based design method
The invention discloses an unmanned aerial vehicle integrated computer, a computer-based control system and a computer-based design method; a computer motherboard comprises a processor, a CAN (controller area network) communication circuit, a DI (data input) signal conditioning circuit, a DO (data o...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses an unmanned aerial vehicle integrated computer, a computer-based control system and a computer-based design method; a computer motherboard comprises a processor, a CAN (controller area network) communication circuit, a DI (data input) signal conditioning circuit, a DO (data output) signal conditioning circuit, a PWM/PPM (pulse width modulation and pulse position modulation) captured signal conditioning circuit, a PWM/PPM output signal conditioning circuit, an A/D (analog/digital) converter and signal conditioning circuit, an D/A (digital/analog) converter and signal conditioning circuit, a serial port communication circuit, a GPS (global positioning system) antenna, a measurement and control antenna, a total voltage tube and a static voltage tube; a measurement and control system comprises a measurement and control antenna and a remote control both connected with the computer; a surface inspection system comprises a surface inspection system upper computer connected with the computer. |
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