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基于连通图的高速高机动目标变结构多模型算法 被引量:1

High Speed High Maneuvering Target Variable Structure Multiple Model Algorithm Based on Connected Graph
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摘要 针对传统的基于活跃有向图的变结构多模型(variable structure multiple model based on adaptive digraph,AD-VSMM)算法不能实现模型子集之间快速跳转且计算量大的问题,提出了一种基于连通图的高速高机动目标变结构多模型(variable structure multiple model algorithm based on connected graph,CG-VSMM)算法.通过分析传统AD-VSMM算法的模型集转换方法,选择加速度和角速度作为模型参数,建立模型集连通图之间的连通关系.根据目标机动情况选择参与计算的模型子集,然后依据子模型的后验概率大小对模型子集进行实时局部调整.Monte Carlo仿真结果表明,新方法能实现变结构多模型(variable structure multiple model,VSMM)算法模型子集之间的快速跳转,且跟踪精度、计算量、稳定性等都得到了较好的改善,可应用于高速高机动目标的跟踪. The traditional algorithm of variable structure multiple model based on adaptive digraph (AD- VSMM) cannot quickly jump between model sets, and requires large amount of computation. To deal with the problem, a variable structure multiple model algorithm based on connected graph (CG-VSMM) to the high speed high maneuvering targets is proposed. By analyzing the model sets conversion method of the traditional AD-VSMM, acceleration and angular velocity are selected as the model parameters to establish connectivity relationships between model sets connected graph. Models involved in the calculation are chosen depending on the target tactical situation. Partial models are adjusted according to the posterior probability of sub-model in real time. Monte Carlo simulation results show that the proposed method can achieve quick jump between models of VSMM algorithm. Tracking accuracy, computation complexity, and stability are improved. It can be used to track high speed high maneuvering targets.
出处 《应用科学学报》 CAS CSCD 北大核心 2013年第5期468-474,共7页 Journal of Applied Sciences
基金 国家自然科学基金(No.61271451)资助
关键词 连通图 高速高机动 变结构多模型 跟踪 connected graph, high speed high maneuvering, variable structure multiple model, tracking
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参考文献12

  • 1贺成龙,陈欣,吴了泥.可重复使用运载器上升段飞行控制[J].应用科学学报,2010,28(2):216-220. 被引量:1
  • 2BAHARI M H, PARIZ N, DAVARPANAH S M, TOOSIZADEH S. An intelligent self-tuning ap- proach for high maneuvering target tracking [C]//Proceedings of the International Conference on Computer and Electrical Engineering. Dubai, UAE, 2009: 249-253.
  • 3BAHARI M H, AZEMI A, PARIZ N, KHORASHADI S, MOHSEN S. High maneuvering target tracking using fuzzy fading memory [J]. Information and Control, 2011, 7(2): 182-187.
  • 4DAHMANI M, KECHE M, OUAMRI A, MECHE A. A new IMM algorithm using fixed coefficients filters (fast IMM) [J]. AEU-International Journal of Elec- tronics and Communications, 2010, 64(12): 1123- 1127.
  • 5Qu Hongquan, PANG Liping, Lr Shaohong. A novel interacting multiple model algorithm [J]. Signal Pro- cessing, 2009, 89(11): 2171-2177.
  • 6LI X R, JILKOV V P. A survey of maneuvering target tracking-part V: multiple-model methods [J]. IEEE Transactions on Aerospace and Electronic Systems, 2005, 41(4): 1255-1321.
  • 7LAN Jian, LI Xiaorong, CHUN Dimu. Best model aug- mentation for variable-structure multiple-model es- timation [J]. IEEE Transactions on Aerospace and Electronic Systems, 2011, 47(3): 2008-2025.
  • 8HUANG Xiangyu, PENG Dongliang. The sequential likelihood ratio test VSMM algorithm for maneu- vering target tracking [C]/ /Proceedings of the Inter- national Conference on Intelligent Control and Au- tomation. Jinan, China, 2010: 6864-6867.
  • 9ZHANG Min, CHEN Weidong. Variable structure mul- tiple model particle filter for maneuvering radar tar- get tracking [C]//Proceedings of the International Conference on Microwave and Millimeter Wave Tech- nology. Chengdu, China, 2010: 1754-1757.
  • 10LI X N, QIN Z, CUO R H, L1 G B. A variable- structure IMM filtering algorithm based on current statistical model [C]//Proceedings of the Interna- tional Conference on Mechatronics and Automation. Changchun, China, 2009: 2983-2988.

二级参考文献12

  • 1张子彦.可重复使用空间飞行器的飞行控制[J].北京航空航天大学学报,2003,29(12):1105-1109. 被引量:2
  • 2张庆振,任章.天地往返可重复使用运载器再入飞行GNC系统关键技术[J].航天控制,2006,24(5):27-30. 被引量:7
  • 3SULLIVAN B W B. X-34 Program overview[R]. AIAA, 1998-3516: 149.
  • 4ZHU J J, HUIZENGA A B. X-33 ascent flight control design by trajectory linearization - a singular perturbation approach[R]. AIAA, 2000-4159: 2-3.
  • 5WHORTON M S, HALL C E, COOK S A. Ascent flight control and structural interaction for the ares-I crew launch vehiclelR]. AIAA 2007-1780: 4-6.
  • 6BAHM C, BAUMANN E. The X-43A hyper-X Mach 7 flight 2 guidance, navigation, and control overview and flight test results[R1. AIAA 2005-3275: 1-10.
  • 7HAL C E l, GALLAHER M W, HENDRIX N D. X-33 attitude control system design for ascent, transition, and entry flight regimes[R]. AIAA-98-4411: 1-5.
  • 8HANSON J M, COUGHLIN D J, DUKEMAN G A. Ascent, transition, entry, and abort guidance algorithm design for the X-33 vehicle[R]. AIAA-98-4409: 3-5.
  • 9Wu Xiaofei, ADAM/ T, CAMPBELL J, GUAN Jian- wei, ZHU J J. A nonlinear flight controller design for a UFO by trajectory linearization method part II -controller design[C]//Proceedings of the Thirty- Fourth Southeastern Symposium on System Theory, 2002: 103-107.
  • 10ZHU J J, HUIZENGA A B. A type two trajectory linearization controller for a reusable launch vehicle - a singular perturbation approach[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit; Providence, RI; Aug. 16-19, AIAA, 2004, 5184: 2-3.

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