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Stability Region of Closed-loop Pilot-vehicle System for Fly-by-wire Aircraft Based on Linear Matrix Inequalities
CAO Qimeng, LI Yinghui, XU Haojun
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2013, (1): 19 -27 .  DOI: 10.7527/S1000-6893.2013.0003

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341