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论文:2023,Vol:41,Issue(5):878-886 |
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引用本文： |
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闫斌斌, 林泽淮, 刘双喜, 闫杰. 基于动态逆控制的高超声速飞行器飞/发一体化控制方法研究[J]. 西北工业大学学报 |
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YAN Binbin, LIN Zehuai, LIU Shuangxi, YAN Jie. Research on integrated aircraft-engine control method of hypersonic vehicle based on dynamic inversion control[J]. Journal of Northwestern Polytechnical University |
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| 基于动态逆控制的高超声速飞行器飞/发一体化控制方法研究 |
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| 闫斌斌1, 林泽淮1, 刘双喜2,3, 闫杰4 |
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1. 西北工业大学 航天学院, 陕西 西安 710072;
2. 国防科技大学 空天科学学院, 湖南 长沙 410073;
3. 国防科技大学 高超声速技术实验室, 湖南 长沙 410073;
4. 西北工业大学 无人系统技术研究院, 陕西 西安 710072 |
| 摘要: |
| 为了减小高超声速飞行器飞/发耦合效应对自身的影响,开展了高超声速飞行器飞/发一体化控制研究。建立面向控制的高超声速飞行器飞/发一体化数学模型。分别采用非线性动态逆控制与增量非线性动态逆控制方法,设计了姿态慢变外回路、角速率快变内回路控制算法。基于包含高超声速飞行器飞/发耦合特性的在线本体模型,以操纵交联的形式设计了高超声速飞行器姿态与发动机的耦合控制方案。在非线性动态逆控制器中引入参考模型、误差控制、在线估计等模块,保证了高超声速飞行器的飞行品质和鲁棒性要求。仿真实验结果表明,采用了非线性动态逆控制设计的飞/发耦合控制方案达到了预期的控制性能。 |
| 关键词:
高超声速飞行器
飞/发一体化
非线性动态逆
增量非线性动态逆
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| Research on integrated aircraft-engine control method of hypersonic vehicle based on dynamic inversion control |
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| YAN Binbin1, LIN Zehuai1, LIU Shuangxi2,3, YAN Jie4 |
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1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;
3. Hypersonic Technology Laboratory, National University of Defense Technology, Changsha 410073, China;
4. Unmanned System Research Institute, Northwestern Polytechnical University, Xi'an 710072, China |
| Abstract: |
| In order to reduce the influence of the coupling characteristics between the aircraft and engine of hypersonic vehicle, an integrated aircraft-engine control method of hypersonic vehicle is studied in this paper. Firstly, the control-oriented aircraft-engine integrated mathematical model of the hypersonic vehicle is established. Then, by using the nonlinear dynamic inversion (NDI) and the incremental nonlinear dynamic inversion (INDI), the outer loop control algorithm with slow attitude change and the inner loop control algorithm with fast angular rate change are respectively designed. Moreover, based on the online ontology model including aircraft-engine coupling characteristics of the hypersonic vehicle, the coupling control scheme of flight posture and engine of the hypersonic vehicle is designed in the form of control linkage. Finally, the reference model, error control, online estimation and other modules are introduced into the NDI controller to ensure the flight quality and robustness requirements of the hypersonic vehicle. The simulation results show that the aircraft-engine coupling control scheme based on the NDI achieves the expected control performance. |
| Key words:
hypersonic vehicle
aircraft/engine integration
nonlinear dynamic inversion
incremental nonlinear dynamic inversion
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| 收稿日期: 2022-11-17
修回日期:
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| DOI: 10.1051/jnwpu/20234150878 |
| 基金项目: 国家自然科学基金(62173274)、陕西省自然科学基础研究计划(2020JC-19)、航空科学基金(20200001053005)、中央高校基本科研业务费(D5000220138)与西北工业大学硕士研究生实践创新能力培育基金(PF2023046)资助 |
| 通讯作者: 刘双喜(1995—),国防科技大学博士后,主要从事飞行器制导与控制研究。e-mail:lsxdouble@163.com
Email：lsxdouble@163.com |
| 作者简介: 闫斌斌(1980—),西北工业大学副教授,主要从事飞行器制导与控制研究。
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参考文献: |
|
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[1] DING Yibo, WANG Xiaogang, BAI Yuliang, et al. An improved continuous sliding mode controller for flexible air-breathing hypersonic vehicle[J]. International Journal of Robust and Nonlinear Control, 2020, 30(14): 5751-5772
[2] XU B, SHI Z K. An overview on flight dynamics and control approaches for hypersonic vehicles[J]. Science China Information Sciences, 2015, 58(7): 1-19
[3] 郭宗易, 周军, 郭建国. 高速飞行器新型自适应干扰估计姿态控制律[J]. 西北工业大学学报, 2017, 35(2): 177-182 GUO Zongyi, ZHOU Jun, GUO Jianguo. On a new adaptive disturbance observer-based attitude control[J]. Journal of Northwestern Polytechnical University, 2017, 35(2): 177-182 (in Chinese)
[4] 王冠, 尹童, 曹颖. 国外高超声速武器攻防发展态势研究[J]. 现代防御技术, 2022, 50(2): 26-32 WANG Guan, YIN Tong, CAO Ying. Research on the development of foreign hypersonic offensive and defensive weapons[J]. Modern Defence Technology, 2022, 50(2): 26-32 (in Chinese)
[5] 季春生. 飞发一体化控制先进技术发展分析[J]. 航空动力, 2019(4): 32-38 JI Chunsheng. Analysis to the development of advanced technology for integrated flight-propulsion control[J]. Aerospace Power, 2019(4): 32-38 (in Chinese)
[6] 李宏新, 谢业平. 从航空发动机视角看飞/发一体化问题[J]. 航空发动机, 2019, 45(6): 1-8 LI Hongxin, XIE Yeping. Fundamental issues of aircraft/engine integration from the perspective of aeroengine[J]. Aeroengine, 2019, 45(6): 1-8 (in Chinese)
[7] LI Y, LIU X, HE Q, et al. L1 adaptive structure-based nonlinear dynamic inversion control for aircraft with center of gravity variations[J]. Journal of Intelligent & Robotic Systems, 2022, 106(1): 1-16
[8] KEREAM S S, ABDALLA A N, FRAYYEH H F, et al. Three phase induction motor torque ripple minimization based on a novel nonlinear dynamic inverse controller[C]//Proceedings of the National Conference for Postgraduate Research, 2016: 321-329
[9] 罗飞, 张军红, 王博, 等. 基于非线性动态逆的舰载机直接升力航迹控制[J]. 飞行力学, 2021, 39(1): 40-45 LUO Fei, ZHANG Junhong, WANG Bo, et al. Direct lift trajectory control for carrier aircraft based on NDI[J]. Flight Dynamics, 2021, 39(1): 40-45 (in Chinese)
[10] 杨浩, 裴海龙. 一类输入饱和非仿射非线性系统的非线性动态逆控制[J]. 控制理论与应用, 2021, 38(4): 425-432 YANG Hao, PEI Hailong. Nonlinear dynamic inversion approach for a class of nonaffine nonlinear systems with input saturation[J]. Control Theory & Applications, 2021, 38(4): 425-432 (in Chinese)
[11] 李飞, 李新国. 基于动态逆-滑模的高速飞行器控制器设计[J]. 飞行力学, 2016, 34(2): 64-67 LI Fei, LI Xinguo. Dynamic inversion-sliding mode for breathing hypersonic vehicle controller design[J]. Flight Dynamics, 2016, 34(2): 64-67 (in Chinese)
[12] 张翾, 吴梅, 王宇航. 基于BP神经网络动态逆的纵列式直升机控制[J]. 飞行力学, 2021, 39(6): 36-41 ZHANG Xuan, WU Mei, WANG Yuhang. Tandem helicopter control based on BP neural network dynamic inversion[J]. Flight Dynamics, 2021, 39(6): 36-41 (in Chinese)
[13] 陈阳, 马建伟. 基于非线性干扰观测器的旋转导弹动态逆控制器设计[J]. 火力与指挥控制, 2018, 43(8): 156-159 CHEN Yang,MA Janwei. Dynamic inversion control for spinning missilebased on nonlinear disturbance observer[J]. Fire Control & Command Control, 2018, 43(8): 156-159 (in Chinese)
[14] 党小为, 唐鹏, 孙洪强, 等. 基于角加速度估计的非线性增量动态逆控制及试飞[J]. 航空学报, 2020, 41(4): 193-201 DANG Xiaowei, TANG Peng, SUN Hongqiang, et al. Incremental nonlinear dynamic inversion control and flight test based on angular acceleration estimation[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(4): 193-201 (in Chinese)
[15] PAVEL M D, SHANTHAKUMARAN P, CHU Q, et al. Incremental nonlinear dynamic inversion for the apache AH-64 helicopter control[J]. Journal of the American Helicopter Society, 2020, 65(2): 1-16
[16] 刘安, 余宗金, 廖保全, 等. 四旋翼式飞行潜航器非线性增量动态逆控制[J]. 飞行力学, 2022, 40(2): 67-73 LIU An, YU Zongjin, LIAO Baoquan, et al. Incremental nonlinear dynamic inversion control for aquad-rotor aerial underwater vehicle[J]. Flight Dynamics, 2022, 40(2): 67-73 (in Chinese) |
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