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Robust Flight Control Design for the HIRM based on Linear Quadratic Control

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Keywords: aircraft control; linear quadratic methods; non linearity compensation; parametric uncertainties; proportional integral control; robust control

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S1270-9638(00)01067-1

Affiliations: bCentro Italiano Ricerche Aerospaziali, Via Maiorise, 81043 , Capua (CE), Italy

Publication date: September 1, 2000

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