| 摘要 |
A control system of a pilotless aircraft consists of series-connected a setting unit, a multiplexer, an analog-digital converter, a calculator, a digital-analog converter, a servodrive and an angle sensor and an angular velocity sensor, a voltage sensor, as well as a current sensor. The system additionally contains two angle sensors and two angular velocity sensors, which outputs are connected to fifth, sixth, seventh, eighth normalizing amplifiers. |
