Longitudinal robust autopilot design for air-to-air missile using μ synthesis

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College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [1 ]
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Nanjing Li Gong Daxue Xuebao | 2009年 / 6卷 / 766-769期
关键词：
Flight envelopes - Air navigation - Three term control systems - Uncertainty analysis - Guided missiles - Controllers - Closed loop systems - Longitudinal control;
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