Flexible Launch Vehicle Control Using Robust Observer-Based Controller Obtained through Structured H ∞ Synthesis
2015 ◽
pp. 23-38
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1998 ◽
Vol 21
(3)
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pp. 409-415
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2005 ◽
Vol 13
(3)
◽
pp. 333-347
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1991 ◽
Vol 6
(2)
◽
pp. 23-29
◽
2000 ◽
Vol 23
(6)
◽
pp. 1013-1020
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Keyword(s):
1966 ◽
2002 ◽