| 自抗扰控制技术在某型导弹上的应用 |
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| 引用本文： | 陈新龙,杨涤,耿斌斌. 自抗扰控制技术在某型导弹上的应用[J]. 飞行力学, 2006, 24(1): 81-84 |
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| 作者姓名： | 陈新龙 杨涤 耿斌斌 |
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| 作者单位： | 哈尔滨工业大学,航天工程与力学系,黑龙江,哈尔滨,150001 |
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| 摘 要： | 将自抗扰控制技术用于某型导弹控制系统设计,从工程应用的角度出发,提出了一种内外双闭环自抗扰姿态控制器设计方法,具体论述了设计的方法原理和过程。仿真结果表明,该方法有较强的鲁棒性和适应性,有较好的动态和稳定性能。
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| 关 键 词： | 自抗扰控制 跟踪微分器 状态观测器 |
| 文章编号： | 1002-0853(2006)01-0081-04 |
| 收稿时间： | 2005-03-14 |
| 修稿时间： | 2005-11-18 |
Application of Auto-Disturbance-Rejection-Controller to a Missile |
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| CHEN Xin-long,YANG Di,GENG Bin-bin. Application of Auto-Disturbance-Rejection-Controller to a Missile[J]. Flight Dynamics, 2006, 24(1): 81-84 |
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| Authors: | CHEN Xin-long YANG Di GENG Bin-bin |
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| Affiliation: | Department of Astronautic Engineering, Harbin Institute of Technology, Harbin 150001, China |
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| Abstract: | This paper applied an auto-disturbance-rejection-controller(ADRC) to the missile control system design.A inner-outer double close-loop ADRC attitude controller as viewed from engineering is presented and the design method and process are discussed in detail.The simulation result shows that the design method studied in this paper has stronger robustness,adaptability,better dynamic capability and stability. |
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| Keywords: | auto-disturbance-rejection-controller trackdifferentiator state observer |
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