[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]只测视线角速度的大机动目标状态估计器设计
The Design of State Estimator of Highly Maneuvering Targets from Measure-only Line-of-sight Angular Velocity
Received date: 2010-11-19
Online published: 2025-05-29
田宏亮 , 梁晓庚 , 贾晓洪 , 郭晓楠 . 只测视线角速度的大机动目标状态估计器设计[J]. 弹箭与制导学报, 2012 , 32(1) : 63 -65 . DOI: 10.15892/j.cnki.djzdxb.2012.01.039
For highly maneuvering targets, the target model was built in Cartesian coordinates based on "current" statistical model. Since target state model was linear and measurement model was nonlinear, the two-step filter was used. Adaptive filtering was a-chieved by an online estimation of target acceleration variance and measurement noise variance. For highly maneuvering targets, simulation results show that the estimator's errors can converge more rapidly and are less than EKF estimator's errors. So the tar-get state estimator is applicable to infrared imaging missile for highly maneuvering targets.
| [1] | 周宏任, 敬忠良, 王培德. 机动目标跟踪[M]. 北京: 国防工业出版社, 1991. |
| [2] | Haupt G T, Kasdin N J, Keiser G M, et al. Optimal Recursive iterative algorithm for discrete nonlinear least-squares estimation[J]. Journal of Guidance, Control, and Dynamics, 1996, 19 (3): 643- 649. |
| [3] | Kasdin N J, Haupt G T. Second-order correction and nu-merical considerations for the two-step optimal estimator[J]. Journal of Guidance, Control, and Dynamics, 1997, 20 (2): 362- 369. |
| [4] | Zhou Di, Mu Chundi, Xu Wenli. Adaptive two-step filter with applications to bearings-only mrasurement problem[J]. Journal of Guidance, Control, and Dynamics, 1999, 22 (5): 726- 728. |
| [5] | 王小虎. 先进寻的导弹制导、半实物仿真及相关理论研究[D]. 北京: 北京航空航天大学, 2000. |
| [6] | SONG T L, UMTY. Practical guidance for homing missiles with bearings-only measurements[J]. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32 (1): 434- 443. |
/
| 〈 |
|
〉 |