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论文:2019,Vol:37,Issue(5):962-967 |
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引用本文： |
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张明环, 马万超, 郭云鹤, 徐胜利. 具有鸭舵/尾舵多操纵面的导弹复合控制方法研究[J]. 西北工业大学学报 |
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ZHANG Minghuan, MA Wanchao, GUO Yunhe, XU Shengli. A New Compound Control Method for Missile with Canard and Tail Rudders[J]. Northwestern polytechnical university |
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| 具有鸭舵/尾舵多操纵面的导弹复合控制方法研究 |
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| 张明环1, 马万超2, 郭云鹤3, 徐胜利3 |
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1. 西北工业大学 航天学院, 陕西 西安 710072;
2. 上海航天技术研究院, 上海 201109;
3. 上海机电工程研究所, 上海 201109 |
| 摘要: |
| 提出了一种具有鸭舵/尾舵多操纵面的导弹复合控制方法。首先建立了导弹的数学模型并进行了小扰动线性化，构建了鸭舵/尾舵复合控制系统，基于序列二次规划法设计了鸭舵/尾舵复合分配策略，并在Matlab/Simulink平台上进行了仿真验证。仿真结果表明，设计的鸭舵/尾舵复合控制系统不仅具有良好的动态性能和稳态性能，还能够在减小阻力的同时确保导弹从低空低速到高空高速都具备高机动能力，证明了新算法具有较高的可信性和实用性。 |
| 关键词:
导弹
鸭舵/尾舵
复合控制
序列二次规划
仿真
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| A New Compound Control Method for Missile with Canard and Tail Rudders |
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| ZHANG Minghuan1, MA Wanchao2, GUO Yunhe3, XU Shengli3 |
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1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. Shanghai Academy of Spaceflight Technology, Shanghai 201109, China;
3. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China |
| Abstract: |
| A new compound control method for missile with canard and tail rudders is presented in this paper. Firstly, the mathematical model of missile with canard/tail rudder is built and linearized using the small disturbance method. Then, the canard/tail rudder compound control system is created; the canard/tail rudder compound allocation strategy is designed based on the sequential quadratic programming method. Finally, the compound control method is verified on Matlab/Simulink. The simulation results show that the compound control method can not only ensure the high dynamic and steady state performance of the control system, but also ensure the high maneuverability of the missile in whole airspace with low drag, thus proving the algorithm in this paper to be reliable and effective. |
| Key words:
missile
canard/tail rudder
compound control
sequential quadratic programming
simulation
mathematical model
Matlab/Simulink
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| 收稿日期: 2018-10-20
修回日期:
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| DOI: 10.1051/jnwpu/20193750962 |
| 基金项目: 上海航天科技创新基金（SAST2017-010）资助 |
| 通讯作者:
Email： |
| 作者简介: 张明环(1985-),西北工业大学助理研究员,主要从事制导控制系统设计与仿真研究。
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参考文献: |
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[1] YUN Yuhang, TANG Shengjing, GUO Jie, et al. Robust Controller Design for Compound Control Missile with Fixed Bounded Convergence Time[J]. Journal of Systems Engineering and Electronics, 2019, 29(1):116-133
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[3] WANG Zhengjie, LI Yangbo, LI Jing, et al. Modeling and Combined Control of Aerial Vehicle Based on Aerodynamic Force and Lateral Thrust[C]//The 2010 International Conference on Modelling, Identification and Control, 2010:106-111
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[7] 毕永涛,王宇航,姚郁. 直/气复合控制导弹的模型预测和自抗扰姿态控制设计[J]. 宇航学报, 2015, 36(12):1373-1383 BI Yongtao, WANG Yuhang, YAO Yu. Attitude Control Design of Missiles with Dual Control Based on Model Predictive Control and Active Disturbance Rejection Control[J]. Journal of Astronautics, 2015, 36(12):1373-1383(in Chinese)
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[9] 陈晓,王新民,周健. 基于序列二次规划法优化无人机飞行性能[J]. 计算机仿真, 2012, 29(12):99-102 CHEN Xiao, WANG Xinmin, ZHOU Jian. UAV Flight Performance Optimization Based on Sequential Quadratic Programming Method[J]. Computer Simulation, 2012, 29(12):99-102(in Chinese) |
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