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|標題:||Fuzzy side force control for missile against hypersonic target||作者:||Lin, C.L.
|關鍵字:||guidance law;design||Project:||Iet Control Theory and Applications||期刊/報告no：:||Iet Control Theory and Applications, Volume 1, Issue 1, Page(s) 33-43.||摘要:||
An integrated fuzzy-logic-based missile side force control mechanism is proposed for the interception of ballistic targets in three-dimensional space. Stringent scenarios when the missile intercepts the ballistic target at higher attitudes are considered. Conventional guidance systems with the aerodynamically controlled mechanism alone are usually incapable of engaging a high-speed target at low-air-density layers. To overcome the difficulty because of insufficient manoeuvrability, a fuzzy side force control scheme configured with two additional auxiliary thrusters is proposed to generate extra transverse acceleration and thereby to reinforce the engagement performance. A simulation study proves the effectiveness of the proposed approach.
|Appears in Collections:||電機工程學系所|
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