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531.
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Zhen Xinyan Zhao Wei 《中国航空学报》2007,20(6):529-538
A new algorithm is developed to achieve accurate state estimation in ground moving target tracking by means of using road information. It is an adaptive variable structure interacting multiple model estimator with dynamic models modification (DMM VS-IMM for short). Firstly, road information is employed to modify the target dynamic models used by filter, including modification of state transition matrix and process noise. Secondly, road information is applied to update the model set of a VS-IMM estimator. Predicted state estimation and road information are used to locate the target in the road network on which the model set is updated and finally IMM filtering is implemented. As compared with traditional methods, the accuracy of state estimation is improved for target moving not only on a single road, but also through an intersection. Monte Carlo simulation demonstrates the efficiency and robustness of the proposed algorithm with moderate computational loads. 相似文献
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舰载机斜板滑跃起飞情况地面载荷 总被引:1,自引:0,他引:1
设置舰艏斜板以减少舰载机起飞滑跑距离、降低甲板风要求,从而实现无弹射系统情况下的短距起飞作业,这已在一些“蓝水”海军强国的航空母舰上得到了多年应用。给定航母起飞甲板长度和斜板曲线构型,飞机能否成功滑跃起飞取决于它的气动特性、最大起飞质量、发动机推力、出口速度和起落架强度。
本文提出了一种舰载机斜板滑跃起飞情况地面载荷的计算方法,也建立了完整的斜板曲线方程(曲线已经过飞机适配性优化)。文中还应用本方法计算了某双座多用途舰载教练机的滑跃起飞地面载荷。 相似文献
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Rosetta Ground Segment and Mission Operations 总被引:1,自引:0,他引:1
At the European Space Operations Centre in Darmstadt (Germany) the activities for ground segment development and mission operations
preparation for Rosetta started in 1997. Many of the characteristics of this mission were new to ESOC and have therefore required
an early effort in identifying all the necessary facilities and functions. The ground segment required entirely new elements
to be developed, such as the large deep-space antenna built in New Norcia (Western Australia). The long duration of the journey
to the comet, of about 10 years, required an effort in the operations concept definition to reduce the cost of routine monitoring
and control. The new approaches adopted for the Rosetta mission include full transfer of on-board software maintenance responsibility
to the operations team, and the installation of a fully functioning spacecraft engineering model at ESOC, in support of testing
and troubleshooting activities in flight, but also for training of the operations staff. Special measures have also been taken
to minimise the ground contact with the spacecraft during cruise, to reduce cost, down to a typical frequency of one contact
per week. The problem of maintaining knowledge and expertise in the long flight to comet Churyumov–Gerasimenko is also a major
challenge for the Rosetta operations team, which has been tackled early in the mission preparation phase and evolved with
the first years of flight experience. 相似文献
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研究了二维翼型在移动地面和固定地面条件下的地面效应及流动特性问题.流场求解采用雷诺平均N-S方程,湍流模型采用k-ω和SST模型.对NACA0015对称翼型在离地速度为1 m/s情况下的非定常绕流进行了计算,选取移动地面条件下不同高度的定常解与非定常计算结果进行了比较.结果表明,考虑非定常效应时升力和阻力的变化明显小于定常解的结果,相对而言力矩的差别较小,固定地面条件下的升力系数和阻力系数略大于移动地面条件下的计算结果. 相似文献
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