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dc.contributor.authorNiewhoener, R.J.
dc.contributor.authorKaminer, Isaac
dc.dateMarch-April 1996
dc.date.accessioned2017-04-25T19:06:54Z
dc.date.available2017-04-25T19:06:54Z
dc.date.issued1996-03
dc.identifier.citationR. J. Niewhoener and I. Kaminer, "On Integrated Aircraft/Controller Design Using Linear Matrix Inequalities'', AIAA Journal of Guidance and Control, vol. 19, no.2, pp. 445-452, March-April 1996.
dc.identifier.urihttps://hdl.handle.net/10945/52692
dc.descriptionAIAA Journal of Guidance and Control, vol. 19, no.2, pp. 445-452, March-April 1996.en_US
dc.description.abstractA new methodology is presented for solving the problem of optimizing the aircraft parameters, such as the size of its control surfaces, while meeting open- and closed-loop static and dynamic performance requirements. The approach proposed involves rewriting these requirements as linear matrix inequalities and solving a related constrained optimization problem for which efficient numerical solutions are available.en_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleIntegrated Aircraft-Controller Design Using Linear Matrix Inequalitiesen_US
dc.typeArticleen_US


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