Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/44122
標題: Fuzzy side force control for missile against hypersonic target
作者: Lin, C.L.
林俊良
Wang, T.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.
URI: http://hdl.handle.net/11455/44122
ISSN: 1751-8644
DOI: 10.1049/iet-cta:20045253
Appears in Collections:電機工程學系所

Show full item record
 

Google ScholarTM

Check

Altmetric

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.