| THE DECOUPLING CONTROL FORAIRCRAFT IN RAPID ROLL |
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| 引用本文： | Hu Weiduo,Zhang Minglian,Wen Chuanyuan(Department of Automatic Control,Beijing University of Aeronautics and Astronautics,Beijing,China,100083). THE DECOUPLING CONTROL FORAIRCRAFT IN RAPID ROLL[J]. 中国航空学报, 1994, 0(4) |
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| 作者姓名： | Hu Weiduo Zhang Minglian Wen Chuanyuan(Department of Automatic Control Beijing University of Aeronautics and Astronautics Beijing China 100083) |
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| 作者单位： | Department of Automatic Control，Beijing University of Aeronautics and Astronautics，Beijing，China，100083 |
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| 摘 要： | ＴＨＥＤＥＣＯＵＰＬＩＮＧＣＯＮＴＲＯＬＦＯＲＡＩＲＣＲＡＦＴＩＮＲＡＰＩＤＲＯＬＬＨｕＷｅｉｄｕｏ，ＺｈａｎｇＭｉｎｇｌｉａｎ，ＷｅｎＣｈｕａｎｙｕａｎ（ＤｅｐａｒｔｍｅｎｔｏｆＡｕｔｏｍａｔｉｃＣｏｎｔｒｏｌ，ＢｅｉｊｉｎｇＵｎｉｖｅｒｓｉｔｙｏ...
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THE DECOUPLING CONTROL FORAIRCRAFT IN RAPID ROLL |
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| Hu Weiduo,Zhang Minglian,Wen Chuanyuan. THE DECOUPLING CONTROL FORAIRCRAFT IN RAPID ROLL[J]. Chinese Journal of Aeronautics, 1994, 0(4) |
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| Authors: | Hu Weiduo Zhang Minglian Wen Chuanyuan |
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| Abstract: | The control problem for aircraft in rapid roll is analyzed. A 5-DOF modelis used to derive a decoupling control law of roll, pitch and sideslip angular velocitiesaccording to the nonlinear decoupling theory. The stability of the closed-loop system isdiscussed. A method to stabilize the whole system when some fixed dynamics areunstable is given. Simulations are perfonned. |
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| Keywords: | aireraft nonlinear systems input /output routines deeoupling stability dynamic response |
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