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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 6: 71 - 75

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.06.015

A Transfer Alignment Accuracy Evaluation Method For Helicopter Borne Missile Based on Dual Master INS

  • ZHAO Weigao ,
  • ZHU Qiju ,
  • BAI Liang
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  • Xi'an Modern Control Technology Research Institute,Xi'an 710065,China

Received date: 2020-11-03

  Online published: 2025-02-07

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Abstract

Aiming at the actual engineering application requirements of the transfer alignment accuracy evaluation of helicopter-borne missiles, a transfer alignment accuracy evaluation method based on dual master inertial navigation was proposed. On the premise that the installation error between the two master inertial navigation systems is measurable, the quantitative evaluation of the installation error between the main inertial guide and the projectile inertial guide is realized by estimating the installation error between the reference master inertial guide and the projectile inertial guide. On this basis, the corresponding test scheme is designed and the method is verified, the results show that the method is reasonable and feasible, and has good engineering reference significance.

Key words： helicopter-borne missiles; transfer alignment; dual master inertial navigation; accuracy evaluation

Cite this article

ZHAO Weigao , ZHU Qiju , BAI Liang . A Transfer Alignment Accuracy Evaluation Method For Helicopter Borne Missile Based on Dual Master INS[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(6) : 71 -75 . DOI: 10.15892/j.cnki.djzdxb.2021.06.015

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References

Publishing order | Descend order by publishing year | Descend order by cited within
[1]
王司, 邓正隆. 惯导系统动基座传递对准技术综述[J]. 中国惯性技术学报, 2003, 11(2):63-69.

[2]
韩鹏鑫, 穆荣军, 崔乃刚, 等. 一种动基座传递对准算法性能评估的工程方法[J]. 中国惯性技术学报, 2009, 17(3):272-277.

[3]
王冰玉. 基于多观测量的惯导传递对准精度评估方法[D]. 哈尔滨: 哈尔滨工程大学, 2015.

[4]
YIN H L, XU B, LIU D Z. A comprehensive method for evaluating precision of transfer alignment on a moving base[J]. Journal of Marine Science and Application, 2017(16): 344-351.

[5]
夏家和, 张金亮, 雷宏杰. 一种用于机载导弹动基座传递对准精度分析的工程方法[J]. 上海航天, 2014, 31(1):44-49.

[6]
严恭敏. 捷联惯导算法与组合导航原理[M]. 西安: 西北工业大学出社, 2010:10-11.

[7]
夏家和, 张金亮, 雷宏杰. 一种改进的速度加姿态匹配快速传递对准算法[J]. 中国惯性技术学报, 2017, 25(1):17-21.

[8]
陈勇. 机载战术武器的速度加姿态匹配传递对准技术研究[D]. 哈尔滨: 哈尔滨工业大学, 2017.

[9]
秦永元. 惯性导航[M]. 北京: 科学出版社, 2006:377-378.

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