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Improving missile guidance performance by in-flight two-step nonlinear estimation of radome aberration
Improving missile guidance performance by in-flight two-step nonlinear estimation of radom...
Improving missile guidance performance by in-flight two-step nonlinear estimation of radome aberration

Detailed Information

Material Type  
 기사
ISSN  
10636536
Author  
Pini Gurfil
Title/Author  
Improving missile guidance performance by in-flight two-step nonlinear estimation of radome aberration / Pini Gurfil ; N. Jeremy Kasdin
Publish Info  
New York, NY : Institute of Electrical and Electronics Engineers, 2004.
Material Info  
pp. 532-541
General Note  
Indudes Bibiography Reference
Added Entry-Personal Name  
N. Jeremy Kasdin
Host Item Entry  
IEEE transactions on control systems technology : Vol. 12 No. 4 (2004. 7) 2004, 07
Electronic Location and Access  
 url
모체레코드  
모체정보확인
Control Number  
kjul:60263436

MARC

 008201016s2004        ai                            aa    eng
■022    ▼a10636536
■1001  ▼aPini  Gurfil
■24510▼aImproving  missile  guidance  performance  by  in-flight  two-step  nonlinear  estimation  of  radome  aberration▼dPini  Gurfil▼e  N.  Jeremy  Kasdin
■260    ▼aNew  York,  NY▼bInstitute  of  Electrical  and  Electronics  Engineers▼c2004.
■300    ▼app.  532-541
■500    ▼aIndudes  Bibiography  Reference
■7001  ▼aN.  Jeremy  Kasdin
■773    ▼tIEEE  transactions  on  control  systems  technology▼gVol.  12  No.  4  (2004.  7)▼d2004,  07
■856    ▼uhttps://www.ieee.org
■SIS    ▼aS029539▼b60077650▼h8▼s2▼fP

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