近代航機上的各種電子設備，已不再依賴獨立自主的系統裝置，而是整合成一個數位的電子裝備，在老舊的機種因顧慮到系統諸多的因素故而將其航空電子設備提昇為數位電子的系統，本論文提出一個可行的概念，對於現行機種C-130H以商業技術的加持Commercial Off-The-Shell (COTS)設計一套數位化的飛行面版，籍由參考其它的系統，本論文將以飛行員現行的系統配置來做設計上的考量，最終數位化控制將能夠在系統上發揮最大的效益，在數位電子系統發展過程，軍用規範MIL-Spec 1553資料匯流排實現了操作上數據的交換、傳輸以及存取功能，並靠著多重航空電子次系統的協調聯繫，來分享訊息、統籌運用，憑籍著對數位系統整合的信賴，航空電子數位可以籍由提昇來增加系統的多裕度能力及更佳的可靠度，本研究將以中華民國空軍運輸機種為例，評估目前類比式儀表駕駛艙系統提昇為數位化儀表駕駛艙之可行性，並以C-130機種為參考模式，並且加以考量當前執行任務及飛行性能，加以設計並且評估系統需求，作為日後機型性能提昇之參考依據。

The modern aircraft on a variety of electronic devices, it is no longer relied on the stand-alone system configuration, but becomes an integrated digital avionics. The old aircraft can upgrade their avionics into digital systems by considering numerous factors in system enhancement. This thesis proposes a feasible concept to design a new digital flight panel for C-130 with commercial off-the-shell (COTS) products. By referring to other system upgrade, the design consideration with system configuration for pilot maneuvering is presented in this thesis. Eventually it will take digital control to be able to develop the greatest efficiency on the system. During the development of digital avionic system, MIL-Spec 1553 data bus is introduced to achieve dates exchanged, transmission, access of the operational performance. It relies on the coordination of multiple avionics subsystems to share the messages, coordinately to apply. With the credit of digital system integration, avionics system performance can be enhanced with redundant capability for better reliability. This study will use the Taiwan Air Force Military Aircraft cargo/transporter as case study to evaluate the feasibility current analog instrument system upgrade to glass cockpit system. C-130 is selected as the model of the reference and considers the current characteristics of mission task and flight performance. It will be designed and evaluated the demand of the system and as the reference of the upgraded glass cockpit system in the future.

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