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[an error occurred while processing this directive]LOS Angle Reconstruction and Guidance System Design of Strapdown Seeker Homing Munitions
Received date: 2015-12-29
Online published: 2025-05-30
金国强 , 马清华 , 王萧 , 赵阳阳 , 王龙 . 捷联寻的弹药惯性视线重构及制导系统设计[J]. 弹箭与制导学报, 2016 , 36(5) : 25 -28,32 . DOI: 10.15892/j.cnki.djzdxb.2016.05.007
Detecting information of strapdown seeker was coupled with missile attitude information, so it can't be used for calculating guidance command directly. Based on the downward-looking strapdown homing scheme, the theoretical decoupling model of LOS( line-ofsight) angle from detecting LOS information and missile attitude information was established, as well as its simplified form under rolling stabilizing circumstance. By means of a nonlinear differential filter-tracking differentiator, smooth inertial LOS rate was acquired and a guidance synthetic system of strapdown seeker homing munitions was designed. Trajectory simulation results show that, based on downwardlooking strapdown homing scheme, precise guidance of short-range guided munitions can be accomplished effectively, which has definite value in engineering.
| [1] | 祁载康 制导弹药技术[M]. 北京: 北京理工大学出版社, 2002: 99- 100. |
| [2] | 姚郁, 章国江. 捷联成像制导系统的若干问题探讨[J]. 红外与激光工程, 2006, 35 (1): 1- 6. |
| [3] | VERGEZ P L, MCCLENDON J R. Optimal control and es- timation for strapdown seeker guidance of tactical missiles[J]. Journal of Guidance Control and Dynamics, 2012, 5 (3): 225-226. |
| [4] | 李璟璟. 捷联成像导引头视线角速率估计方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2008. |
| [5] | 韩京清, 王伟. 非线性跟踪微分器[J]. 系统科学与数学, 1994, 14(2): 177-183. |
| [6] | 武利强, 林浩, 韩京清. 跟踪微分器滤波性能研究[J]. 系统仿真学报, 2004, 16(4): 651-652. |
| [7] | KIM D, RYOO C K, KIM Y, et al. Guidance and control for missiles with a strapdown seeker[C] // Proc. of the American Institute of Aeronautics and Astronautics Guid-ance, Navigation, and Control Conference, 2010: 2-5. |
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