Proceedings of the 2003 American Control Conference, 2003.
DOI: 10.1109/acc.2003.1239715
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MIMO control system design for aircraft via convex optimization

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Cited by 2 publications
(4 citation statements)
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“…The aircraft demonstrated advanced fighter technologies that have been used in the development of many modern high performance military aircraft. A linear model was obtained by trimming the aircraft at 25000 feet altitude and 0.9 Mach speed (Cifdaloz et al, 2003). This linear model is a MIMO model having an unstable phugoid mode.…”
Section: The Himat Research Aircraftmentioning
confidence: 99%
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“…The aircraft demonstrated advanced fighter technologies that have been used in the development of many modern high performance military aircraft. A linear model was obtained by trimming the aircraft at 25000 feet altitude and 0.9 Mach speed (Cifdaloz et al, 2003). This linear model is a MIMO model having an unstable phugoid mode.…”
Section: The Himat Research Aircraftmentioning
confidence: 99%
“…where W 1 and W 2 are the weights which provide a reference singular value response according to defined specifications. Appropriate values for the weights were also taken from Cifdaloz et al (2003).…”
Section: Design Specificationsmentioning
confidence: 99%
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“…This approach is now being utilized for practical applications, particularly in the flight control area (O. Cifdaloz et al (2003); O. Voinot et al (2003); G. Ferreres and G. Puyou (2006)).…”
Section: Multiobjective Design Via Q-parametrizationmentioning
confidence: 99%