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Fan Shipeng, Lin Defu, Wang Jinran, Wang Wei. Error analysis and correction for hardware-in-the-loop simulation system of laser guidance weapon[J]. Infrared and Laser Engineering, 2013, 42(4): 904-908.
Citation: Fan Shipeng, Lin Defu, Wang Jinran, Wang Wei. Error analysis and correction for hardware-in-the-loop simulation system of laser guidance weapon[J]. Infrared and Laser Engineering, 2013, 42(4): 904-908.

Error analysis and correction for hardware-in-the-loop simulation system of laser guidance weapon

  • Received Date: 2012-08-11
  • Rev Recd Date: 2012-09-13
  • Publish Date: 2013-04-25
  • According to the characteristic of laser guided weapon, a hardware-in-the-loop simulation (HILS) model for guidance and control system was founded. Then, all kinds of errors impacting on simulation system, especially geometric error, were analyzed, and a guidance model with error was created. Through the mathematic simulation, the maximal angle error was given to limit miss distance within allowable range. In order to correct the geometric error, a model of HILS was developed for seeker to track a certain laser spot on curtain. Using the obtained results, nonlinear over determined equations of error parameters were established. With combination of Newton iteration method and weighted least square method, the error parameters were solved and geometric model was corrected accurately. The results indicate that this approach has achieved exceptional accuracy and reliability, which is significant for next phase of HILS.
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    [2] Wang Jiang, Lin Wei, Wang Peng, et al. Analysis of laser energy chain in the hardware-in-the-loop simulation system of semi-active laser guidance[J]. Infrared and Laser Engineering, 2011, 40(7): 1230-1233. (in Chinese)
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    [4] Zhang Hongxi. Analysis of influence induced by installation error of seeker in hardware-in-the-loop simulation[J]. Computer Emulation, 2010, 27(12): 31-34. (in Chinese)
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    [6] Meng Xiuyun, Liu Zaozhen, Wang Zhaomin, et al. Error analysis and modeling of a hardware-in-the-loop simulation system of laser-guided bombs[J]. Computer Emulation, 2002, 19(2): 7-9. (in Chinese)
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    [8] Xiao Weiguo, Hao Chong'en, Li Gaofeng. Research on error for a three-axis flight simulation turntable[J]. Journal of System Simulation, 2001, 13(5): 678-680. (in Chinese)
    [9] Xiao Weiguo, Er Lianjie. Error analysis of radar guidance hardware-in-loop simulation[J]. Journal of System Simulation, 2007: 6. (in Chinese)
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    [11] Meng Daikui. Effect of turntable errors on the hardware-in-the-loop simulations of spinning missiles[J]. Aerospace Control, 1992, (3): 57-61. (in Chinese)
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    [13] Bi Ye. Error analysis of missile's hardware-in-loop simulation system[D]. Xi'an Northwestern polytechnic University, 2006. (in Chinese)
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    [15] Garnell P. Guided Weapon Control Systems, Second Revision by Qi Zaikang[M]. Beijing: Institute of Technology, 2004: 88-95.
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    [17] Mou Yu, Lin Defu, Qi Zaikang, et al. Performance of proportional navigation law for terminal laser-guided projectile[J]. Infrared and Laser Engineering, 2009, 38(2): 250-255. (in Chinese)
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Error analysis and correction for hardware-in-the-loop simulation system of laser guidance weapon

  • 1. School of Aerospace Science,Beijing Institute of Technology,Beijing 100081,China;
  • 2. College of Art and Design,Beijing Institute of Technology,Beijing 100081,China

Abstract: According to the characteristic of laser guided weapon, a hardware-in-the-loop simulation (HILS) model for guidance and control system was founded. Then, all kinds of errors impacting on simulation system, especially geometric error, were analyzed, and a guidance model with error was created. Through the mathematic simulation, the maximal angle error was given to limit miss distance within allowable range. In order to correct the geometric error, a model of HILS was developed for seeker to track a certain laser spot on curtain. Using the obtained results, nonlinear over determined equations of error parameters were established. With combination of Newton iteration method and weighted least square method, the error parameters were solved and geometric model was corrected accurately. The results indicate that this approach has achieved exceptional accuracy and reliability, which is significant for next phase of HILS.

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