Discrete time multiple spacecraft formation flying attitude optimal control in presence of relative state constraints

This paper addresses the challenge of synchronized multiple spacecraft attitude reorientation in presence of pointing and boundary constraints with limited inter-spacecraft communication link. Relative attitude pointing constraint among the fleet of spacecraft has also been modeled and considered during the attitude maneuvers toward the desired states. Formation fling control structure that consists of decentralized path planners based on virtual structure approach joint with discrete time optimal local controller is designed to achieve the mission’s goals. Due to digital computing of spacecraft’s onboard computer, local optimal controller based on discrete time prediction and correction algorithm has been utilized. The time step of local optimal algorithm execution is designed so that the spacecraft track their desired attitudes with appropriate error bound. The convergence of the proposed architecture and stability of local controller’s tracking error within appropriate upper bound are proved. Finally, a numerical simulation of a stereo imaging scenario is presented to verify the performance of the proposed architecture and the effectiveness of the algorithm.     

相关进近模式的近距平行跑道尾流危险区域分析

相比于机场一起一降的运行模式,近距平行跑道的相关平行进近运行模式可以最大限度地提升跑道容量.根据尾流在大气中各个阶段的运动特性,得到了以时间为变量的尾流水平侧移距离数学模型.应用Matlab仿真软件得到了侧风及地面效应影响情况下的上海虹桥国际机场实行近距平行跑道相关平行进近的侧向尾流危险区域图,并分析得到了后机不受到前机尾流影响情况下两机需保持26.9 s的最大尾流时间间隔.利用尾流危险区域的特点,可缩短尾流时间间隔,从而大幅度提高机场容量.     

基于概率极限状态的RAIM风险评估

为了提供准确可靠的完好性服务,提出了基于概率极限状态的RAIM完好性风险评估。考虑所需导航性能参数和噪声的因素,建立了安全系数与可靠系数相结合的完好性风险评估指标体系,确立风险评价准则。非精密进近的算例分析表明,系统评估方法是可行的且有效的。     

关于进行程序管制一体化模拟练习的设想

在程序管制模拟练习中,存在着塔台管制服务、进近管制服务和区域管制服务互不衔接,不能系统地模拟整个管制过程的问题。针对这一情况提出了程序管制一体化模拟练习和程序和管制一体化模拟机的结构设计。     

Spatial approaches to moons from resonance relative to invariant manifolds

In this study, the final approach to a moon or other body from resonance is explored and compared to the invariant manifolds of unstable periodic orbits. It is shown that the stable manifolds of planar Lyapunov orbits can act as a guide for the periods or resonances that are required for the final approach in both the planar and spatial problems. Previously developed techniques for the planar problem are expanded for use with resonances and used for comparison with trajectories approaching a moon from these resonances. A similar technique is then used for exploring the relationship of invariant manifolds to approach trajectories in the spatial problem. It is shown that the invariant manifolds of unstable periodic orbits provide insight into the trajectory design, and they can be used as a guide to the more direct approach trajectories.     

联合优化的BP神经网络模型的应用研究

BP算法因收敛速度慢、易于陷入局部极小值等缺点，使得对于较大的搜索空间、多峰值和不可微函数常常不能搜索到全局极小点，这些制约了BP网络在各个领域中的应用。本文通过对学习系数、神经元的激励函数及误差函数的联合优化，在一定程度上避免了学习中的局部极小问题，提高了学习效率，改进了网络的性能。     

基于局部均值分解和峭度图的滚动轴承包络分析方法

提出了基于局部均值分解(local mean decomposition,LMD)和峭度图(kurtogram)的滚动轴承包络分析方法.该方法中,原始滚动轴承故障振动信号通过LMD进行自适应的频率成分分离和初步降噪,包络分析中带通滤波器的参数通过峭度图客观地提供,从而提高滚动轴承包络分析的准确度.通过对滚动轴承仿真信号以及实验信号的分析,结果表明:在低信噪比情况下,LMD可以自适应分离出滚动轴承的固有振动成分,峭度图可以自动确定包络分析中带通滤波器的参数,与传统包络分析比较,所提方法能更加清晰准确地提取滚动轴承的故障特征.      

涡轮叶片CT图像边缘提取的最优算子研究

为了解决叶片计算机断层(computed tomograghy,简称CT)图像边缘提取精度低效率差的问题,以解析法提取边缘的理论为基础,推导了适用于CT图像边缘提取的最优算子,并通过定量计算与模拟标准图像对最优算子的性能进行了分析,结果表明最优算子在抗噪、定位精度以及单像素响应等方面都比传统的边缘提取算子更为优越.实际应用最优算子提取的叶片边缘更光顺,噪声点以及伪边缘更少,进一步证明了最优算子在CT图像边缘提取方面有着明显的优势.      

局部附面层吸除对高负荷扩压叶栅气动性能的影响

实验研究了低速条件下局部附面层吸除对高负荷扩压叶栅气动性能的影响.采用五孔气动探针测量了叶栅出口截面气动参数,并对叶片表面静压进行了测量,详细分析了局部吸气方式、吸气量和吸气位置对叶栅出口截面总压损失和负荷能力的影响.结果表明,采用吸力面两端吸气和中间吸气方式均能够有效吸除叶栅流道内低能流体,增加叶栅的气动负荷,从而提高叶栅的气动性能;采用吸力面两端吸气对叶栅气动性能的改善要优于吸力面中间吸气;叶栅气动性能的改善主要在靠近叶展中部区域,而对角区核心区和端部区域的影响并不明显.      

止裂孔尺寸对止裂效果影响的研究

当航空器结构在航线使用过程中出现疲劳裂纹损伤时,通常在裂纹尖端打止裂孔进行临时性修理。通过理论分析和计算及试验分析,研究了止裂孔尺寸对止裂效果的影响。结果表明,当航空器结构出现疲劳裂纹损伤时,采用5.57～7.14mm直径的止裂孔进行止裂修理,止裂效果较好;当止裂孔直径为6.35mm时,止裂效果最好。