| 变结构自适应控制在BTT导弹中的应用 |
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| 引用本文： | 周军,陈新海,冯文剑,郑焕敏.变结构自适应控制在BTT导弹中的应用[J].航空学报,1994,15(8):988-992. |
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| 作者姓名： | 周军 陈新海 冯文剑 郑焕敏 |
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| 作者单位： | 西北工业大学航天工程学院，北京电子系统工程研究所 |
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| 摘 要： | 提出了ＢＴＴ导弹自动驾驶仪的变结构自适应设计方法。该方法完全基于对象参数变化和随机扰动的上下界,无需对系统进行参数辩识和对随机扰动进行在线估计,增强了控制系统的适应性和鲁棒性。在考虑了各种非理想因素的情况下,得到了令人满意的仿真结果。
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| 关 键 词： | 变化－结构分析 模型参考自适应控制 转弯飞行 自动驾驶仪 |
THE APPLICATION OF VARIABLE STRUCTURE MODEL REFERENCE ADAPTIIVE CONTROL FOR BANK-TO-TURN MISSILES |
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| ZhouJun, Chen Xinhai.THE APPLICATION OF VARIABLE STRUCTURE MODEL REFERENCE ADAPTIIVE CONTROL FOR BANK-TO-TURN MISSILES[J].Acta Aeronautica et Astronautica Sinica,1994,15(8):988-992. |
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| Authors: | ZhouJun Chen Xinhai |
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| Institution: | 1. Astronautical Engineering Institute,Northwestern Polytechnical University,Xian,710072;2. Beijing Insitute of Electronic System Engineering,Beijing,100854 |
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| Abstract: | new variable structure model referenee adaptive control method is proposed for bank-to-turn (BTT)missiles’roll channel autopilot designs.The method is completely based on the maximums and the minimums of plant’s parameter variations and random disturbances,and avoids utilizing on-line parameter identification and on-line random disturbance estimation,which improves the adaptivity and robustness of control systems.With many non-ideal factors taken into account,satisfactory digital simulation results are presented. |
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| Keywords: | variations-structure analysis model reference adaptive control turning flight automatic pilots |
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