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|標題:||A dynamically fuzzy gain - scheduled design for missile autopilot||作者:||Lin, C.L.
|關鍵字:||h-infinity control||Project:||Aeronautical Journal||期刊/報告no：:||Aeronautical Journal, Volume 107, Issue 1076, Page(s) 599-606.||摘要:||
A dynamic backpropagation training algorithm for an adaptive fuzzy gain scheduling feedback control scheme with the application to missile autopilots is developed. This novel design methodology uses a Takagi-Sugeno fuzzy system to represent the fuzzy relationship between the scheduling variables and controller parameters. Mach number and angle-of-attack are used as measured, time-varying exogenous scheduling variables injected into the control law. By incorporating scheduling parameter variation information, the adaptation law for controller parameters is derived. Results from extensive simulation studies show that the presented approach offers satisfactory controlled system performance.
|Appears in Collections:||電機工程學系所|
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