不完全线性约束下的状态估计

Yuan Huang, Xueying Wang, Yulan Guo, W. An
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引用次数: 5

摘要

研究了一个带目标约束的状态估计问题。反辐射导弹(ARM)通常沿着X-Y平面上几乎是线性的弹道向目标移动。轨迹和目标位置的线性约束被称为先验约束,可以用来提高跟踪滤波器的性能。本文首先对目标约束卡尔曼滤波器(DCKF)进行了改进。然后,提出了两种通过估计轨迹斜率来融合先验知识的方法。在第一种方法中,每次使用无约束卡尔曼滤波器估计的点和目标点直接估计斜率。在第二种方法中,使用最小二乘法来估计所有测量值的斜率。几种有效的线性等式约束状态估计方法可以利用估计的斜率和目标点。建立了一个典型的ARM跟踪场景来测试所提出的卡尔曼滤波器。本文还对近年来的研究进行了全面的比较,包括无约束非线性滤波方法和后向Cramer-Rao下界(PCRLB)。蒙特卡罗仿真结果说明了该方法在目标约束下状态估计的有效性。
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State estimation with incomplete linear constraint
A problem of state estimation with destination constraint is considered in this paper. An anti-radiation missile (ARM) often moves towards the target along a trajectory which is almost linear in the X-Y plane. The linear constraint for trajectory and target position are known as priori and can be used to enhance the performance of a tracking filter. In this paper, a destination constrained Kalman filter (DCKF) is first revised for our problem. Then, two methods are proposed to incorporate the prior knowledge by estimating the slope of the trajectory. In the first method, the slope is estimated directly at each time using the point estimated by a unconstrained Kalman filter and the destination point. In the second method, a least square method is used to estimate the slope from all measurements. Several effective linear equality constrained state estimation methods can be used to exploit the estimated slop and the destination point. A typical ARM tracking scenario is established to test the proposed Kalman filter. A comprehensive comparison to recent work is also presented, including unconstrained nonlinear filtering methods and the Posterior Cramer-Rao Lower Bound (PCRLB). Monte-Carlo simulation results are presented to illustrate the effectiveness of the proposed methods for state estimation with destination constraint.
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