本論文針對無人飛行載具，對其的航電系統做一統整，包括機上的電子載具系統，與地面站兩個部份，在機上的電子載具包括了Auto Pilot與攝影功能，地面包括了資料監控與事後資料分析的部份。更進一步的將GPS與INS以卡曼濾波器(Kalman Filter)做整合，且在導引部份加入最小功率平飛轉彎的應用，且對整個航電的設計與製作留下完整的記錄，方便事後能重新製作與改進。 This paper presents the Integrated Avionic System of Unmanned Aerial Vehicle (UAV), include electronic system on plane which have both auto pilot and CCD and ground station which have both monitor plane data and analysis. Also use Kalman Filter integrates GPS and INS. Apply optimal level turn. Record all documents that are design and produce avionic system of unmanned aerial vehicle.
