排序方式: 共有25条查询结果,搜索用时 412 毫秒
1.
2.
3.
4.
5.
本文考虑了杂波环境下机动目标的多雷达跟踪问题,提出了一种分布式联合估计算法。子站独立于总站,并单独跟踪,把当地估计结果周期地传送给总站,由总站进行合并,得出基于所有子站量测的全局估计。数字仿真表明,分布式联合、估计算法在各种性能指标上都优于单站跟踪算法。 相似文献
6.
7.
8.
飞行器易损性指标计算的基本理论与方法(Ⅱ) 总被引:4,自引:0,他引:4
文章是飞行器易损性指标计算基本理论的第二部分。在第一部分给出的单次击中易损性指标计算公式的基础上, 研究了多次击中情况下飞行器易损性指标计算的两种方法, 并给出了相应的计算公式。最终通过具体的算例说明了方法的有效性 相似文献
9.
This paper develops a modular modeling and efficient formulation of launch dynamics with marching fire (LDMF) using a mixed formulation of the transfer matrix method for multibody systems (MSTMM) and Newton-Euler formulation. Taking a ground-borne multiple launch rocket systems (MLRS), the focus is on the launching subsystem comprising the rocket, flexible tube, and tube tail. The launching subsystem is treated as a coupled rigid-flexible multibody system, where the rocket and tube tail are treated as rigid bodies while the flexible tube as a beam with large motion. Firstly, the tube and tube tail can be elegantly handled by the MSTMM, a computationally efficient order-N formulation. Then, the equation of motion of the in-bore rocket with relative kinematics w.r.t. the tube using the Newton-Euler method is derived. Finally, the rocket, tube, and tube tail dynamics are coupled, yielding the equation of motion of the launching subsystem that can be regarded as a building block and further integrated with other subsystems. The deduced dynamics equation of the launching subsystem is not limited to ground-borne MLRS but also fits for tanks, self-propelled artilleries, and other air-borne and naval-borne weapons undergoing large motion. Numerical simulation results of LDMF are given and partially verified by the experiment. 相似文献
10.