為了達到小型飛機依靠航電系統的自主性飛行，現代的電子資訊技術是一個絕佳的實現方法。衛星定位系統固然可以提供長週期穩定的導航定位，然而衛星定位系統的可用性尚無法達到飛航要求，因此一個全功能的自主性飛行系統可以用來提升衛星定位系統的可用性。在本文中，整合了衛星定位系統、慣性量測系統以及大氣數據系統，以及包含了從基本分析到實現的即時飛行控制系統，成為一個自主性飛行系統。在自主性飛行系統中，利用微處理器設計方法整合了各個次系統，而在飛行控制系統中的核心為ARM微處理器，藉由處理上傳以及下載的飛行資訊，提供載具完整的飛行狀態資訊。文中所設計的自主性飛行系統，從設計製造到實現，並利用載具作完整有效地測試、修正與分析。

To aim on an independent avionics system for small aircrafts, modern delicate electronic devices may be the most feasible candidate to adopt. Since GPS is a good solution for long term navigation, however, the GPS availability can not meet aviation requirement. A full function of flight autonomous system may need to enhance the navigation capability using alternative availability technologies. In this dissertation, an integration of flight autonomous system to include GPS, INS, ADU, as well as a remote flight control system is proposed with fundamental analysis and system implementation. In the flight autonomous system, microprocessor-based design is introduced to include more functions into one small system. In the remote flight control system, ARM CPU is built to manipulate information uplink and downlink for better awareness of airborne conditions. The overall system has been designed and fabricated with some feasible tests to support the proposed system in completeness and effectiveness.

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