| 飞机横侧向系统的INA设计和鲁棒性分析 |
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| 引用本文： | 马晓军,程鹏.飞机横侧向系统的INA设计和鲁棒性分析[J].航空学报,1993,14(9):550-555. |
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| 作者姓名： | 马晓军 程鹏 |
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| 作者单位： | 北京航空航天大学301教研室，北京航空航天大学301教研室 北京，100083，北京，100083 |
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| 摘 要： | 用INA方法设计某飞机的横侧向控制系统,数学仿真的结果说明针对高度H=10 000m,Ma为0.9的飞行状态设计的横侧向控制器同样适用于高度H=10 000m,Ma为1.5的飞行状态。最后用鲁棒INA方法对设计进行了鲁棒性分析,说明该设计提高了模型误差可允许的界限。
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| 关 键 词： | 对角优势 鲁棒性 鲁棒对角优势 |
AN INA DESIGN AND ROBUST ANALYSIS OF THE LATERAL FLIGHT CONTROL SYSTEM |
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| Ma Xiao-jun,Cheng Peng.AN INA DESIGN AND ROBUST ANALYSIS OF THE LATERAL FLIGHT CONTROL SYSTEM[J].Acta Aeronautica et Astronautica Sinica,1993,14(9):550-555. |
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| Authors: | Ma Xiao-jun Cheng Peng |
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| Institution: | Faculty 301 oj Beijing University of Aeronautics and Astronautics, Beijing, 100083 |
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| Abstract: | In this paper, the lateral flight control system is designed in INA methodology. The result of simulation shows that the lateral controler designed for H= 10 000 metres, Ma = 0.9 can be used in the situation of H= 10 000 metres, Ma=1.5. Finally, robust analysis is done in robust INA methodology, which shows that the design enhances the admissible bound of the model error. All data are calculated by IBM PC computer. Gershgorin bands, Ostrowski bands and robust Gershgorin bands, robust Ostrowski bands are drawn by MP 1000 drawing instrument. |
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| Keywords: | diagonal dominance robust robust diagonal dominance |
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