Advanced Search
Volume 31 Issue 05
May  2005
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2005  >  31(05): 535-538.
Zhang Jianguo. First-Order Second-Moment Reliability Method and Its Software[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 605-606. (in Chinese)
Citation: Fan Yuezu, Zhang Yinan, Ma Haokai, et al. Application of the hybrid BP/GA algorithm in simple integrated navigation system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(05): 535-538. (in Chinese)
shu

Application of the hybrid BP/GA algorithm in simple integrated navigation system

  • 1.

    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. China Astronautic Science and Industry Company, Beijing 100830, China

  • Received Date: 09 Dec 2003
  • Publish Date: 31 May 2005
    Abstract
  • Kalman filter is the most usual optimization filter with some limitation when applied in the integrated navigation system. Especially in simple global positioning system/ dead reckoning system (GPS/DRS ),the receiver and the inertial navigation units are low-cost and low-accuracy. To improve accuracy of the system, it must be focused on the advanced algorithm. To compensate the divergence of Kalman filter, a hybrid algorithm composed of back propagation (BP) neural net and genetic algorithm (GA) together with Kalman filter was applied in low-cost GPS/DRS integrated navigation system. This algorithm owns not only self-study ability and good real-time performance of neural net but also optimization assessment ability of Kalman filter, and even overcomes many flaws of neural net,such as slow convergence ,sensitivity about the study parameters and local extremums. The simulation result also proves that this algorithm is prior in precise and stability compared to usual Kalman filter, for example, the statistic analysis shows that the maximal error of latitude is reduced to a lower magnitude.

     

    • FullText(HTML)
    • References(1)
  • [1] 韩明华,袁乃昌．多层神经网络在跟踪式Kalman滤波器中的应用[J]．国防科技大学学报,1997,19 (5):18~24 Han Minghua,Yuan Naichang．A improved tracking Kalman filter using a multilayed neural network[J]．Journal of National University of Defense Technology,1997,19 (5):18~24(in Chinese) [2] 庄朝文.车载GPS/DRS/MM组合导航系统应用研究 ．北京:北京航空航天大学自动化科学与电气工程学院,2003 Zhuang Chaowen,Application study on vehicle GPS/DRS/MM integrated navigation system ．Beijing:School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics,2003(in Chinese) [3] 杨朋林,贺 新．人工神经网络与遗传算法结合的研究[J]．现代电子技术,2002,143(12):105~107 Yang Penglin,He Xin．Research on the combination of artificial neural net and genetic algorithm[J]．Modern Electronic Technology,2002,143(12):105~107(in Chinese) [4] 王小平,曹立明．遗传算法——理论、应用于软件实现[M]．西安:西安交通大学出版社,2002.1~4,10~16 Wang Xiaoping, Cao Liming．Genetic agorithm——theory, application and software realization[M]．Xi’an:Xi’an Jiaotong University Press,2002.1~4,10~16(in Chinese) [5] Wu Guangning, Jiang Xiongwei, Xie Hengkun. A neural network used for PD pattern recognition with genetic algorithm ．Proceedings of the 6th International Conference on Properties and Applications of Dielectric Materials . Xi'an:IEEE Inc, 2000.451~454 [6] 王宏伦,吕庆风．模糊逻辑系统GA＋BP混合学习算法[J]．控制理论与应用,2001,18(1):18~20 Wang Honglun,Lü Qingfeng．A hybrid GA-BP self-learning algorithm for fuzzy logic system[J]．Control Theory and Application,2001,18(1):18~20(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]GUO Z，ZHAO G，FU B，et al. Considering visual search characteristics on command and control system KLSM[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2819-2825 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2024.0120.
    [2]LI W，CHENG X，LI Y J. Integrated security control of industrial cyber-physical systems based on new type ADETCS[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2704-2716 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0734.
    [3]WANG H B，HE H，ZOU H J，et al. Nonlinear backstepping control of special EHA for rail grinding vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2439-2448 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0681.
    [4]FANG Y F，WU D Y，LIU T，et al. Model predictive current control of asynchronous motor in rolling mill based on sliding mode theory[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3382-3390 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0576.
    [5]LIN Junting, CHEN Xinzhou. Sliding mode control of magnetic levitation ball systems based on high-gain disturbance observer[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0518
    [6]QUAN Q，CHEN L. Control of non-affine nonlinear systems: A survey[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2367-2381 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0642.
    [7]MENG Z P，YANG L Q，WANG B，et al. ADRC design for folding wing vehicles based on improved equilibrium optimization algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2449-2460 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0698.
    [8]ZHAO J K，GUO H，XU J Q. High performance control method for galvanometer laser scanner system[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3208-3218 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0790.
    [9]LIU H，HUANG S，TU H Y. Quadrotor sliding mode control based on predefined time[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1665-1674 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0481.
    [10]CAI H，SHI P. Attitude control method for flexible spacecraft based on LPV model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3921-3929 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0880.
    [11]JIN L，YANG S L. Fault-tolerant control of spacecraft attitude with prescribed performance based on reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2404-2412 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0666.
    [12]SUN X M，MA X，LIU Y，et al. Adaptive sliding mode region reaching control for uncertain nonlinear systems[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2482-2491 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0647.
    [13]YAN H B，XU W B，HUANG L E. Design of quadrotor attitude controller based on improved ADRC[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3283-3292 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0129.
    [14]WANG S Y，ZHANG J，YANG L Y. Attitude control law based on L1-ITD for a tail-sitter UAV[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2501-2509 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0681.
    [15]WANG T，JIAO H C，LIU J，et al. Design of attitude control method for ultra-low-orbit satellite with pneumatic steering gear[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：548-558 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0265.
    [16]WANG C Y，YANG L M，LI Y H. A mapping leader formation control strategy for multiple mobile robots based on two-stage sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3108-3114 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0792.
    [17]XU Meng, LI Yan, GAO Jie, XU Hai, GAO Bing. Design of aircraft anti-skid braking system integrated sliding mode control based on novel convergence law[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.1085
    [18]ZHANG K Q，ZHOU X F，MEN X H，et al. Three-dimensional integrated guidance and control design with fixed-time convergence[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：842-852 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0360.
    [19]HE J J，YUAN C Q，GONG S P，et al. Sliding mode control for formation flying near libration points using hybrid propulsion[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1222-1230 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0420.
    [20]PAN Chang-zhong, HE Guang, LI Zhi-jing, ZHOU Lan, XIONG Pei-yin. Adaptive Filtered Control for Uncertain Electro-hydraulic Servo Systems with Time-varying Output Constraints[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022-0497
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2639) PDF downloads(193) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return