高动态目标拦截弹制导与控制前沿技术展望Prospect on advanced technology of interceptor guidance and control in high dynamic target defense
周池军,邵雷,骆长鑫,李明杰,雷虎民
摘要(Abstract):
临近空间高动态飞行器武器化进程日益加速,给国家空天安全带来了新的威胁和挑战。临近空间防御作战是应对高动态目标威胁的有效手段,但是对拦截弹的制导控制技术提出了更高的要求。针对临近空间防御作战背景和需求,聚焦拦截弹制导控制过程中涉及的目标轨迹预测、中制导弹道生成与修正、中末制导交接班、精确末制导以及高性能控制5项前沿技术,梳理总结了相关研究的最新进展情况,分析了现有研究的局限性,展望了相关技术的发展方向并给出了可行的研究思路。
关键词(KeyWords): 高动态目标;轨迹预测;中制导;中末制导交接班;末制导;复合控制
基金项目(Foundation): 国家自然科学基金(61873278;62173339)
作者(Author): 周池军,邵雷,骆长鑫,李明杰,雷虎民
DOI: 10.16338/j.issn.2097-0714.20220614
参考文献(References):
- [1]Bertin J J,Cummings R M.Fifty years of hypersonics:Where we’ve been,where we’re going[J].Progress in Aerospace Sciences,2003,39:511-536.
- [2]Morelli E A.Flight-test experiment design for characterizing stability and control of hypersonic vehicles[J].Journal of Guidance,Control,and Dynamics,2009,32(3):949-959.
- [3]吴颖川,贺元元,贺伟,等.吸气式高超声速飞行器机体推进一体化技术研究进展[J].航空学报,2015,35(1):245-260.
- [4]吴立刚,安昊,刘健行,等.吸气式高超声速飞行器控制的最新研究进展[J].哈尔滨工业大学学报,2016,48(10):1-16.
- [5]雍恩米,钱炜棋,何开锋.基于雷达跟踪仿真的滑翔式再入弹道突防性能分析[J].宇航学报,2012,33(10):1370-1376.
- [6]雍恩米,钱炜祺,唐伟,等.考虑禁飞圆的滑翔式机动弹道与气动特性参数耦合设计[J].航空学报,2013,34(1):66-75.
- [7]Li F,Xiong J J,Qu Z G,et al.A damped oscillation model for tracking near space hypersonic gliding targets[J].IEEE Transactions on Aerospace and Electronic Systems,2019,55(6):2871-2890.
- [8]Nemeth C,Fearnhead P,Mihaylova L.Sequential Monte Carlo methods for state and parameter estimation in abruptly changing environments[J].IEEETransactions On Signal Processing,2015,62(5):1245-1255.
- [9]Lim J,Kim H,Park H.Interactive-multiple-model algorithm based on minimax particle filtering[J].IEEESignal Processing Letters,2020,27:36-40.
- [10]李世杰,雷虎民,周池军,等.基于控制变量估计的高超声速再入滑翔目标轨迹预测算法[J].系统工程与电子技术,2020,42(10):2320-2327.
- [11]程云鹏,孙成志,闫晓东.基于SVM和EKF的高超声速滑翔飞行器轨迹预报[J].北京航空航天大学学报,2020,46(11):2094-2105.
- [12]张凯,熊家军,李凡,等.基于意图推断的高超声速滑翔目标贝叶斯轨迹预测[J].宇航学报,2018,39(11):1258-1265.
- [13]孟克子,周荻.多约束条件下的最优中制导律设计[J].系统工程与电子技术,2016,38(1):116-122.
- [14]孙勇,张卯瑞,梁晓玲.求解含复杂约束非线性最优控制问题的改进Gauss伪谱法[J].自动化学报,2013,39(5):672-678.
- [15]张恒浩.基于自适应Radau伪谱法的再入段轨道设计算法[J].北京理工大学学报,2018,38(10):1037-1045.
- [16]任鹏飞,王洪波,周国峰.基于自适应伪谱法的高超声速飞行器再入轨迹优化[J].北京航空航天大学学报,2019,45(11):2257-2265.
- [17]Rahimi A,Kumar K D,Alighanbari H.Particle swarm optimization applied to spacecraft reentry trajectory[J].Journal of Guidance,Control,and Dynamics,2013,36(1):307-310.
- [18]Zhou H Y,Wang X G,Cui N G.Glide trajectory optimization for hypersonic vehicles via dynamic pressure control[J].Acta Astronautica,2019,164:376-386.
- [19]Zhou J,Lei H M,Zhai D L,et al.Optimal midcourse trajectory cluster generation and trajectory modification for hypersonic interceptions[J].Journal of Systems Engineering and Electronics,2017,28(6):1162-1173.
- [20]Li N B,Lei H M,Zhou J,et al.Variable-timedomain online neighboring optimal trajectory modification for hypersonic interceptors[J].International Journal of Aerospace Engineering,2017(4):1-12.
- [21]Zhou J,Lei H M,Zhang D Y.Online optimal midcourse trajectory modification algorithm for hypersonic vehicle interceptions[J].Aerospace Science and Technology,2017,63(4):266-277.
- [22]Mondal S,Padhi R.Angle-constrained terminal guidance using quasi-spectral model predictive static programming[J].Journal of Guidance Control&Dynamics,2017(2):1-9.
- [23]雷虎民,王华吉,邵雷,等.反临近空间高超声速目标拦截弹中末制导交接班窗口[J].国防科技大学学报,2018,40(5):1-8.
- [24]雷虎民.导弹制导与控制原理(修订2版)[M].北京:国防工业出版社,2018.
- [25]张大元,雷虎民,李海宁,等.复合制导导引头开机截获概率估算[J].固体火箭技术,2014,37(2):150-155.
- [26]赵丹,伍建辉,张都川.制导火箭弹中末交接班雷达导引头截获概率分析[J].火控雷达技术,2017,46(4):24-27.
- [27]张锦林,李炯,雷虎民,等.有限过载的三维现实真比例导引的捕获区域[J].系统工程与电子技术,2022,44(3):986-997.
- [28]李万礼,李炯,雷虎民,等.基于滑模变结构制导律的捕获区分析[J].系统工程与电子技术,2021,43(11):3321-3329.
- [29]毛柏源,李君龙,张锐,等.拦截高速机动目标的捕获区及微分对策导引律[J].国防科技大学学报,2021,43(3):165-174.
- [30]杨源.临近空间拦截器末制导及控制问题研究[D].哈尔滨:哈尔滨工业大学,2018.
- [31]胥彪.输入受限的敏捷型导弹制导与控制方法[D].哈尔滨:哈尔滨工业大学,2015.
- [32]张宽桥,刘连照,马晖,等.考虑攻击角约束和输入饱和的制导控制一体化设计[J].弹道学报,2021,33(3):9-18.
- [33]于江龙,董希旺,李清东,等.拦截机动目标的分布式协同围捕制导方法[J/OL].航空学报,1-20[2021-12-08].http://kns.cnki.Net/kcms/detail/11.1929.v.20210817.1013.010.html.
- [34]陈中原,韦文书,陈万春.基于强化学习的多发导弹协同攻击智能制导律[J].兵工学报,2021,42(8):1638-1647.
- [35]Kanellakopoulos I,Kokotovic P,Morse A S.Systematic design of adaptive controller for feedback linearizable systems[J].IEEE Transactions on Automatic Control,1991,36(11):1241-1253.
- [36]Xu B,Zhang Y.Neural discrete back-stepping control of hypersonic flight vehicle with equivalent prediction model[J].Neurocomputing,2015,154:337-346.
- [37]Liu X,Huang W,Du L.An integrated guidance and control approach in three-dimensional space for hypersonic missile constrained by impact angles[J].ISATransactions,2017:164-175.
- [38]Zhao B,Xu S,Guo J,et al.Integrated strapdown missile guidance and control based on neural network disturbance observer[J].Aerospace science and technology,2019,84(1):170-181.
- [39]Zhuang H X,Sun Q L,Chen Z Q,et al.Active disturbance rejection control for attitude control of missile systems based on back-stepping method[J].International Journal of Control Automation and Systems,2021,19(11):3642-3656.
- [40]Wu L G,Shi P,Su X J.Sliding mode control of uncertain parameter-switching hybrid systems[M].London:Wiley,2014.
- [41]郭超,梁晓庚,王俊伟,等.临近空间拦截弹的非奇异终端滑模控制[J].宇航学报,2015,36(1):58-67.
- [42]Ma Q,Jin Y Q.Supersonic missile control with PIsliding mode method[J].Advanced Materials Research,2011,295-297:1773-1776.
- [43]Zhao H C,Zhou H Q,Song Z Q.Smooth second sliding mode control for supersonic missile based on extended state observer[J].2015 International Conference on Automation,Mechanical and Electrical Engineering(AMEE2015).
- [44]Shtessel Y,Yu P,Mehta S S,et al.Air breathing hypersonic missile continuous higher order sliding mode control for maximum target penetration[C].International Workshop on Variable Structure Systems.IEEE,2014.
- [45]Ra C,Kim S,Suk J,et al.Adaptive sliding mode autopilot design for skid-to-turn missile model with uncertainties[J].IFAC Proceedings Volumes,2013,46(19):330-335.
- [46]Hu X X,Guo Y,Zhang L X,et al.Fuzzy stable inversion-based output tracking for nonlinear nonminimum phase system and application to FAHVs[J].Journal of the Franklin Institute,2015,352(12):5529-5550.
- [47]Bu X W,Wu X Y,Ma Z,et al.Novel adaptive neural control of flexible air-breathing hypersonic vehicles based on sliding mode differentiator[J].Chinese Journal of Aeronautics,2015,28(4):1209-1216.
- [48]Xu B,Zhang Q,Pan Y P.Neural network based dynamic surface control of hypersonic flight dynamics using small-gain theorem[J].Neurocomputing,2016,173:690-699.
- [49]Tong W,Wang Q,Dong C Y.Adaptive neural network control based on nonlinear disturbance observer for BTTmissile[C].Control Conference,IEEE,2013.
- [50]Hu Y,Jing L.Robust adaptive controller design for missile with three-tunnel input unmodeled dynamics and uncertainties[C].Control&Decision Conference,IEEE,2010.
- [51]Guo J,Peng Q,Guo Z.SMC-based integrated guidance and control for beam riding missiles with limited LBPU[J].IEEE Transactions on Aerospace and Electronic Systems,2021,57(5):2969-2978.
- [52]Sun R,Na J,Zhu B.Robust approximation-free prescribed performance control for nonlinear systems and its application[J].International Journal of Systems Science,2017,49(2):1-12.
- [53]Zhang Z H,Ma K M.Prescribed performance-based adaptive sliding mode control for the autopilot design of missile with lateral jets[J].Proceedings of the institution of mechanical engineers part g-journal of aerospace engineering,2021-09,doi:10.1177/09544100211044387.(Submitted)
- [54]王刚,李为民,郭相科,等.临空高超声速飞行器威胁防御概论[M].北京:解放军出版社,2017:84-88.
- [55]周池军,李明杰,雷虎民.临近空间再入滑翔目标轨迹预测研究进展综述[J].飞航导弹,2021(6):127-132.
- [56]叶泽浩,毕红葵,段敏,等.控制律预测的再入滑翔飞行器轨迹预测算法[J].现代防御技术,2018,46(6):7-14.
- [57]邵雷,雷虎民,赵锦.临近空间高超声速飞行器轨迹预测方法研究进展[J].航空兵器,2021,28(2):34-39.
- [58]杜润乐,刘佳琪,李志锋,等.基于制导律识别的远期飞行轨迹预测[C].第17届中国系统仿真技术及其应用学术年会,西安,2016:264-268.
- [59]Xie Y F,Zhuang X B,Xi Z P,et al.Dual-channel and bidirectional neural network for hypersonic glide vehicle trajectory prediction[J].IEEE Access,2021(9):92913-92924.
- [60]Zhou J,Lei H M.Coverage-based cooperative target acquisition for hypersonic interceptions[J].Science China Technological Sciences,2018,61(10):1575-1587.
- [61]Zhou J,Lei H M,Zhang D Y.Online optimal midcourse trajectory modification algorithm for hypersonic vehicle interceptions[J],Aerospace Science and Technology,2017,63:1-12.
- [62]张涛,李为民,李炯,等.面向中末交接班的临近空间拦截弹弹道优化[J].宇航学报,2021,42(3):367-377.
- [63]Wang H J,Lei H M,Ye J K,et al.A novel capture region of retro proportional navigation guidance law for intercepting high-speed nonmaneuvering targets[J].Proceedings of the Institution of Mechanical Engineers,2018,232(6):1186-1198.
- [64]Wang H J,Zhang D Y,Zhang T,et al.Capturability analysis of pure proportional navigation guidance law for intercepting hypersonic targets[C].2018 IEEE CSAAGuidance,Navigation and Control Conference(GNCC),IEEE,2018.
- [65]Xu G,Sun K,Liu H.Optimal control of missile interception process based on adaptive dynamic programming[C].2019 Chinese Automation Congress(CAC),IEEE,2020.
- [66]Sun J,Liu C.Disturbance observer-based robust missile autopilot design with full-state constraints via adaptive dynamic programming[J].Journal of the Franklin Institute,2018,355(5):2344-2368.