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论文:2020,Vol:38,Issue(1):170-175 |
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引用本文： |
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王凡, 李宏君, 许红羊, 闫杰, 张进. 考虑进气道不起动的高超声速飞行器鲁棒自适应控制研究[J]. 西北工业大学学报 |
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WANG Fan, LI Hongjun, XU Hongyang, YAN Jie, ZHANG Jin. Robust Adaptive Control of Hypersonic Vehicle Considering Inlet Unstart[J]. Northwestern polytechnical university |
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| 考虑进气道不起动的高超声速飞行器鲁棒自适应控制研究 |
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| 王凡1, 李宏君2, 许红羊1, 闫杰1, 张进3 |
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1. 西北工业大学 航天学院, 陕西 西安 710072;
2. 西安航天动力研究所, 陕西 西安 710072;
3. 上海机电工程研究所, 上海 201109 |
| 摘要: |
| 针对吸气式高超声速飞行器进气道不起动引起飞行器气动特性大范围变化，从而导致响应出现大幅振荡甚至控制系统失稳的问题，提出了一种考虑进气道不起动影响的模型参考自适应控制方法。该方法首先针对进气道起动时的模型，设计了基于LQR-PI方法的姿态控制系统，并以此作为进气道不起动时的参考模型；当进气道不起动时，在LQR-PI基准控制器的基础上增加模型参考自适应控制项，通过跟踪参考模型以提高系统对进气道不起动引起模型偏差的鲁棒性，在进气道出现不起动的情况下能快速稳定姿态，为进气道再起动提供条件。最后对所提方法进行了数字仿真，结果表明，系统在进气道出现不起动时能够快速跟踪控制指令，且稳态误差趋于零，验证了所提方法的有效性。 |
| 关键词:
高超声速飞行器
进气道不起动
模型参考自适应控制
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| Robust Adaptive Control of Hypersonic Vehicle Considering Inlet Unstart |
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| WANG Fan1, LI Hongjun2, XU Hongyang1, YAN Jie1, ZHANG Jin3 |
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1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. Xi'an Aerospace Propulsion Institute, Xi'an 710072, China;
3. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China |
| Abstract: |
| A large-scale change in the aerodynamic characteristics of the aircraft caused by the inlet unstart of the air-breathing hypersonic vehicle causes a large oscillation of the response or even a control system instability. A model reference adaptive control method considering the influence of inlet unstart is proposed. Firstly, the attitude control system is designed based on LQR-PI method for the model of inlet start, which is used as the reference model. When the inlet unstart, the model reference adaptive control is added on the basis of LQR-PI controller to improve the robustness of the system to the uncertainties caused by the inlet unstart. The method can quickly stabilize the attitude when the inlet unstart, and provides conditions for the inlet restart. Finally, the present method is verified by the simulation results. The simulation results show that when the inlet unstart, the system can re-track quickly the control command, and the steady-state error tends to zero, which verifies the effectiveness of the present method. |
| Key words:
air-breathing hypersonic vehicle(AHV)
inlet unstart
model reference adaptive control
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| 收稿日期: 2019-02-24
修回日期:
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| DOI: 10.1051/jnwpu/20203810170 |
| 通讯作者:
Email： |
| 作者简介: 王凡(1991-),女,西北工业大学博士研究生,主要从事飞行器制导控制技术研究。
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| 作者相关文章 |
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| 王凡 在本刊中的所有文章 |
| 李宏君 在本刊中的所有文章 |
| 许红羊 在本刊中的所有文章 |
| 闫杰 在本刊中的所有文章 |
| 张进 在本刊中的所有文章 |
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参考文献: |
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[1] 罗金玲. 高超声速飞行器机体/推进一体化设计的启示[J]. 航空学报. 2015, 36(1):39-48 LUO Jinling. Inspiration of Hypersonic Vehicle with Airframe/Propulsion Integrated Design[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):39-48(in Chinese)
[2] 谭慧俊, 卜焕先, 张起帆,等. 高超声速进气道不起动问题的研究进展[J]. 南京航空航天大学学报, 2014, 46(4):501-508 TAN Huijun, BU Huanxian, ZHANG Qifan, et al. Review of Hypersonic Inlet Unstart Phenomenon[J]. Journal of Nanjing University of Aeronautics&Astronautics, 2014, 46(4):501-508(in Chinese)
[3] 李留刚, 谭慧俊, 孙姝, 等. 二元高超声速进气道不起动状态的信号特征及预警[J]. 航空学报, 2010, 31(12):2324-2331 LI Liugang, TAN Huijun, SUN Shu, et al. Signal Characteristics and Prediction of Unstarting Process for Two-Dimensional Hypersonic Inlet[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(12):2324-2331(in Chinese)
[4] 王晨曦, 谭慧俊, 张启帆,等. 高超声速进气道低马赫数不起动和再起动试验[J]. 航空学报, 2017, 38(11):121146 WANG Chenxi, TAN Huijun, ZHANG Qifan, et al. Test of Low Mach Number Unstart and Restart Process of Hypersonic Inlet[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(11):121146(in Chinese)
[5] 郭帅涛, 李祝飞, 高文智,等. 攻角与马赫数对进气道起动特性的可比拟性[J]. 推进技术, 2017, 38(5):983-991 GUO Shuaitao, LI Zhufei, GAO Wenzhi, et al. Analogy between Effects of Attack Angle and Mach Number on Inlet Starting[J]. Journal of Propusion Technology, 2017, 38(5):983-991(in Chinese)
[6] HUTCHINS E, AKELLA R, CLEMENS T. Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart[C]//AIAA Flow Control Conference, 2012
[7] PETTINARI S, CORRADINI M L, SERRANI A. Detection of Scramjet Unstart in a Hypersonic Vehicle Model[C]//American Control Conference, 2012
[8] SHADAB M A, BAIG M F. Investigation and Control of Unstart Phenomenon in Scramjets[C]//AIAA International Space Planes and Hypersonic System and Technologies Conference, 2017
[9] BOLENDER M A, WILKIN H, JACOBSEN L, et al. Flight Dynamics of a Hypersonic Vehicle during Inlet Un-Start[C]//AIAA International Space Planes and Hypersonic System and Technologies Conference, 2009
[10] LAVRETSKY E, WISE K A. Robust and Adaptive Control with Aerospace Applications[M]. London:Springer, 2013 |
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