| Citation: | ZHOU Rui, ZHANG Yuhang, XIONG Wei, et al. A reentry steady glide guidance algorithm based on fuzzy control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(2): 197-206. doi: 10.13700/j.bh.1001-5965.2020.0264(in Chinese)
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Considering the periodic oscillation in reentry glide of Lifting Hypersonic Vehicle (LHV), a feedback correction method based on fuzzy logic and fuzzy control is proposed to reduce the oscillation and keep reentry glide trajectory smooth. First, the longitudinal guidance is developed based on the prediction of the landing error and the correction of the guidance command, and a fuzzy controller whose input consists of altitude ratio and airspeed is applied to outer loop of the bank angle control system. Then, the lateral guidance is designed by the course angle error corridor and bank reversal logic, which realizes the lateral controls in large transverse range conditions. This method is independent of Quasi-Equilibrium Glide Condition (QEGC) and the problem of parameters design in parametric feedback law is avoided, which enhances the adaptive ability. Based on LHV model, the numerical simulations show that periodic oscillation is effectively reduced by the fuzzy feedback control law within terminal and reentry corridor constraints. Meanwhile, the Monte Carlo simulation with random dispersions and errors verifies the robustness of the proposed algorithm.
| [1] |
LU P. Entry guidance: A unified method[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(3): 713-728. doi: 10.2514/1.62605
|
| [2] |
WANG Y Y, YANG X X, YAN H C. Reliable fuzzy tracking control of near-space hypersonic vehicle using aperiodic measurement information[J]. IEEE Transactions on Industrial Electronics, 2019, 66(12): 9439-9447. doi: 10.1109/TIE.2019.2892696
|
| [3] |
WANG F, GUO Y, WANG K, et al. Disturbance observer based robust backstepping control design of flexible air-breathing hypersonic vehicle[J]. IET Control Theory and Applications, 2019, 13(4): 572-583. doi: 10.1049/iet-cta.2018.5482
|
| [4] |
VOLAND T, HUEBNER D, MCCLINTON R. X-43A hypersonic vehicle technology development[J]. Acta Astronautica, 2006, 59(1): 181-191. http://www.sciencedirect.com/science/article/pii/S0094576506001184
|
| [5] |
谢愈, 刘鲁华, 汤国建, 等. 多约束条件下高超声速滑翔飞行器轨迹优化[J]. 宇航学报, 2011, 32(12): 2499-2504. https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201112007.htm
XIE Y, LIU L H, TANG G J, et al. Trajectory optimization for hypersonic glide vehicle with multi-constraints[J]. Journal of Astronautics, 2011, 32(12): 2499-2504(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201112007.htm
|
| [6] |
徐明亮, 陈克俊, 刘鲁华, 等. 高超声速飞行器准平衡滑翔自适应制导方法[J]. 中国科学: 技术科学, 2012, 42(4): 378-387. https://www.cnki.com.cn/Article/CJFDTOTAL-JEXK201204004.htm
XU M L, CHEN K J, LIU L H, et al. Quasi-equilibrium gliding adaptive guidance method for hypersonic vehicles[J]. Scientia Sinica Technologica, 2012, 42(4): 378-387(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JEXK201204004.htm
|
| [7] |
熊子豪, 任章, 江若冲, 等. 标准轨迹制导中准平衡滑翔条件优化研究[J]. 导航定位与授时, 2016, 3(4): 47-52. https://www.cnki.com.cn/Article/CJFDTOTAL-DWSS201604009.htm
XIONG Z H, REN Z, JIANG R C, et al. Demonstration and improvement of quasi-equilibrium glide condition in reference trajectory reentry guidance[J]. Navigation, Position and Timing, 2016, 3(4): 47-52(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-DWSS201604009.htm
|
| [8] |
赵汉元. 航天器再入制导方法综述[J]. 航天控制, 1994, 1(1): 26-33. https://www.cnki.com.cn/Article/CJFDTOTAL-HTKZ401.004.htm
ZHAO H Y. A survey of guidance methods for spacecraft reentry[J]. Aerospace Control, 1994, 1(1): 26-33(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HTKZ401.004.htm
|
| [9] |
赵江, 周锐. 基于倾侧角反馈控制的预测校正再入制导方法[J]. 兵工学报, 2015, 36(5): 823-830. https://www.cnki.com.cn/Article/CJFDTOTAL-BIGO201505009.htm
ZHAO J, ZHOU R. Predictor-corrector reentry guidance based on feedback bank angle control[J]. Acta Armamentarii, 2015, 36(5): 823-830(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-BIGO201505009.htm
|
| [10] |
赫泰龙, 陈万春, 刘芳. 高超声速飞行器平稳滑翔弹道扰动运动伴随分析[J]. 北京航空航天大学学报, 2019, 45(1): 109-122. doi: 10.13700/j.bh.1001-5965.2017.0545
HE T L, CHEN W C, LIU F. Adjoint analysis of steady glide trajectory with disturbance motion for hypersonic vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(1): 109-122(in Chinese). doi: 10.13700/j.bh.1001-5965.2017.0545
|
| [11] |
梁子璇, 任章. 基于在线气动参数修正的预测制导方法[J]. 北京航空航天大学学报, 2013, 39(7): 853-857. https://bhxb.buaa.edu.cn/CN/Y2013/V39/I7/853
LIANG Z X, REN Z. Predictive reentry guidance with aerodynamic parameter online correction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(7): 853-857(in Chinese). https://bhxb.buaa.edu.cn/CN/Y2013/V39/I7/853
|
| [12] |
JOSHI A, SIVAN K. Predictor corrector reentry guidance algorithm with path constraints for atmospheric entry vehicles[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(5): 1307-1318. doi: 10.2514/1.26306
|
| [13] |
雍恩米, 刘深深, 程艳青, 等. 面向弹道优化的高超声速再入飞行器模态稳定性分析[J]. 航空学报, 2019, 40(7): 42-51. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201907004.htm
YONG E M, LIU S S, CHENG Y Q, et al. Mode stability analysis of hypersonic reentry vehicle for trajectory optimization[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(7): 42-51(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201907004.htm
|
| [14] |
WAN Z J, LIU L, TANG G, et al.Optimal guidance with multi-targets for hypersonic vehicle in dive phase[C]//20136th International Conference on Recent Advances in Space Technologies(RAST).Piscataway: IEEE Press, 2013: 13710685.
|
| [15] |
WANG H L, HUA Y Z, LI Q D.Constrained predictor corrector entry guidance for common aero vehicle[C]//Chinese Control Conference(CCC), 2015: 934-1768.
|
| [16] |
王智, 唐硕, 闫晓东. 高超声速滑翔飞行器约束预测校正再入制导[J]. 飞行力学, 2012, 30(2): 175-180. https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201202022.htm
WANG Z, TANG S, YAN X D. Constrained predictor-corrector reentry guidance for hypersonic glide vehicle[J]. Flight Dynamics, 2012, 30(2): 175-180(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201202022.htm
|
| [17] |
XI Y, MENG Y. Adaptive actuator failure compensation control for hypersonic vehicle with full state constraints[J]. Aerospace Science and Technology, 2019, 85: 464-473. doi: 10.1016/j.ast.2018.12.032
|
| [18] |
GILEFERNANDEZ J, TIERNO M. Practical method for optimization of low-thrust transfers[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(6): 1927-1931. doi: 10.2514/1.50739
|
| [19] |
梅映雪, 冯玥, 王容顺, 等. 高超声速飞行器多约束再入轨迹快速优化[J]. 宇航学报, 2019, 40(7): 758-767. https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201907004.htm
MEI Y X, FENG Y, WANG R S, et al. Fast optimization of reentry trajectory for hypersonic vehicles with multiple constraints[J]. Journal of Astronautics, 2019, 40(7): 758-767(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201907004.htm
|
| [20] |
王青, 莫华东, 吴振东, 等. 考虑禁飞圆的高超声速飞行器再入预测制导[J]. 哈尔滨工业大学学报, 2015, 47(2): 104-109. https://www.cnki.com.cn/Article/CJFDTOTAL-HEBX201502019.htm
WANG Q, MO H D, WU Z D, et al. Predictive reentry guidance for hypersonic vehicles considering no fly zone[J]. Journal of Harbin Institute of Technology, 2015, 47(2): 104-109(in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HEBX201502019.htm
|
| [21] |
管萍, 和志伟. 高超声速飞行器姿态的自适应模糊滑模控制[J]. 控制工程, 2018, 25(7): 1139-1144. https://www.cnki.com.cn/Article/CJFDTOTAL-JZDF201807001.htm
GUAN P, HE Z W. Adaptive fuzzy sliding mode control for hypersonic vehicle attitude[J]. Control Engineering of China, 2018, 25(7): 1139-1144(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JZDF201807001.htm
|
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