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- W221385565 abstract "ABSTRACT The analysis of an aircraft flight dynamics is recently very co nvenient because of the introduction of state-space method and a well-developed package software. The representation of a dynamic system is described as a simple for m of matrix calculation and the unique form of model is available for the linear or nonline ar, time variant or time invariant, mono variable or multi variable system with state-space method. And this analysis can be simplified with the specific functions of a pac kage software and it is very simplified to execute the simulation of the dynamic characteris tics for an aircraft model with an interactive graphical treatment. The purpose of this st udy is to develope an educational flight simulator for the students who need to analy ze the dynamic characteristics of an aircraft that is primarily to execute the simulation for the analysis of the transient response and frequency response of an aircraft stability. Furthermore the dynamic characteristics of an aircraft motion is set up as dynamical animation tool for the control response on 3-axis motions of an aircraft. Key Words : State-Space(상태․공간), Dynamic Characteristic(동특성). Transient Response(과도응답), Frequency Response(주파수 응답), Aircraft Stability(항공기 안정성), Flight Simulator(비행 시뮬레이터)" @default.
- W221385565 created "2016-06-24" @default.
- W221385565 creator A5012860507 @default.
- W221385565 date "2009-01-01" @default.
- W221385565 modified "2023-09-24" @default.
- W221385565 title "Development of the Educational Simulator for Aircraft Dynamic Characteristic Analysis with the State-Space Method" @default.
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