| Summary: | 碩士 === 國立成功大學 === 電機工程研究所 === 84 === The purpose of this research is to develop a flight instrument
software for a PC-based flight simulator which has been
emphasized gradually over the past year in our country. A
generalized software to visualize the behavior of a flight
simulator through cockpit instruments are designed and
developed. The thesis uses two programming languages, LabVIEW
and C language running on Windows operating system and DOS
system, respectively, to simulate aircraft instruments which
include airspeed indicator, Machmeter, altimeter, rate of climb
indicator, attitude director indicator(ADI), and horizontal
situation indicator(HSI) and control panel of an airplane. We
also apply the animation technology and mouse function to raise
its reality and interactive ability. Moreover, the flight
instrument software is also integrated with navigation system
data, air-data computer system data, and aircraft database to
achieve flight simulation function. Finally, three flight modes
are simulated, which are ''Constant Climb Angle Mode'''', ''''OFF
Mode'''', and ''''HDG Mode'''',respectively.
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