Digital Aircraft Instrument System of Ultralight Aircraft with Digital Avionic

• Main Authors: Thai-Peng Chen, 陳在鵬
• Other Authors: Chin.E Lin
• Format: Others
• Language: zh-TW
• Published: 2004
• Online Access: http://ndltd.ncl.edu.tw/handle/33489079813697181204

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 93 === 　Ultralight sport has become more and more popular brings huge opportunities in entertainment business. When people enjoy this entertainment, the flight safety must be considered in full. As far as instruments of ultralight aircraft, they almost are analogy. Their defects are too expensive and poor operation effect. In this thesis, we try design the digital aircraft instrument to join the new avionic data bus system. In this thesis, the proposed digital aircraft instrument is designed to meet ultralight aircraft demands. 　The proposed data bus system is called hybrid data bus (HDB), which is designed and fabricated for test as a preliminary solution. In addition to data bus system, a virtual flight instrument with geographic information system (GIS) is integrated into cockpit display together with mobile communication surveillance for low altitude flight. The overall system design will bring in new era of digital avionics for small aircrafts.