| Summary: | 碩士 === 國立成功大學 === 航空太空工程學系 === 88 === Abstract
This thesis contains two parts: developing an unmanned airship system, and the derivation of a simplified airship model and control.
Control system is the center of the whole unmanned aerial vehicle system. There are two parts in our control system: Onboard flight control system and the human interface. Both of them are PC-based system, and we can change their behavior or what they look like by modifying the software.
The most difference between our control system and others is the force feedback joy stick. We apply this joy stick as the main input device, and simulate the force by the data received from the vehicle. Our goal is to make the pilot feel as if he is on the vehicle.
At the last, we build a simplified model of the airship from dynamics. Then, we estimate the parameters from the experiment, Computer Aid Design, and the relative data from other airships. We use pole-placement method to design the control law. The result are simulated by computer.
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