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Robust controller design for a skid to turn missile

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Title Robust controller design for a skid to turn missile
 
Creator SREENATHA, AG
RAJHANS, V
BHARDWAJ, N
 
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Description The design and analysis of Robust Autopilot for skid-to-turn missile is presented. Two of the popular Robust Controller design approaches, The Loop Shaping Design Procedure (LSDP) and The Robust Eigenstructure Assignment are considered. The missile model considered in the present work is having lightly damped modes and non-minimum phase zeros, with stringent performance requirements. Numerical results are presented to evaluate the Robustness of stability and performance of the controller. Merits and demerits of the above said methodologies are brought out clearly as applied to this specific plant. (C) 1999 . .
 
Publisher PERGAMON-ELSEVIER SCIENCE LTD
 
Date 2011-08-26T08:33:48Z
2011-12-26T12:57:22Z
2011-12-27T05:47:29Z
2011-08-26T08:33:48Z
2011-12-26T12:57:22Z
2011-12-27T05:47:29Z
1999
 
Type Article
 
Identifier ACTA ASTRONAUTICA, 45(2), 85-92
0094-5765
http://dx.doi.org/10.1016/S0094-5765(99)00107-1
http://dspace.library.iitb.ac.in/xmlui/handle/10054/11252
http://hdl.handle.net/10054/11252
 
Language en