调制型光纤捷联系统系泊状态标校方法

针对舰船系泊状态特有的运动环境及惯性器件偏差对捷联系统导航精度的影响,提出一种单轴四位置旋转调制方案并建立该系统误差方程。研究了直观分析系统参数可观测性的解析方法,并运用谱条件数法计算出惯性测量单元（inertial measurement unit, IMU）在静止和旋转状态下各状态量的可观测度,利用分离位置回路的卡尔曼滤波模型实现了器件偏差的现场估计。数值仿真显示,单轴四位置转停方案可以有效地提高惯性器件偏差的可观测度,大大提高了系泊状态下惯性器件偏差的估计精度。     

临近空间慢速平台SAR结合运动补偿的SCFT算法

针对临近空间慢速平台SAR轨迹运动偏差的空变性进行了分析.在二维频率域利用系统传输函数(STF)和变尺度傅里叶变换(SCFT)处理算法有效补偿了距离迁移和关于快时间波数的高阶相位,指出在运动补偿过程中,可将轨迹运动偏差分解成空不变项和空变项.在二雏频率域,结合一阶、二阶运动误差补偿的方法,提出了临近空间慢速平台SAR结合运动补偿的SCFT处理算法.最后,通过计算机仿真,验证了本算法的正确性.     

Optimal maintenance and replacement of extraction machinery

This paper considers a problem of optimal preventive maintenance and replacement schedule of equipment devoted to extracting resources from known deposits. Typical examples are oil drills, mine shovels, etc. At most one replacement of the existing machinery by a new one is allowed. The problem is formulated as an optimal control problem subject to the state constraint that the remaining deposit at any given time is nonnegative. We show that the optimal preventive maintenance, production rates, and the replacement and salvage times of the existing machinery and the new one, if required, can be obtained by solving sequentially a series of free-end-point optimal control problems. Moreover, an algorithm based on this result is developed and used to solve two illustrative examples.     

一类不确定非线性系统的自适应模糊控制

对一类不确定非线性系统提出自适应模糊控制方法。此方法用模糊逻辑系统设计自适应模糊监督控制器和自适应模糊控制器,且设计补偿器对逼近误差进行补偿,以此来减少逼近误差对跟踪精度的影响,同时对自适应模糊监督控制器和自适应模糊控制器中的未知参数设计了自适应学习律。证明了该方法不但能保证闭环系统稳定,而且可使跟踪误差收敛到原点的邻域内。仿真结果验证了此方法的有效性。     

基于改进的圆投影向量的背景补偿方法

针对传统运动背景补偿算法难以适应大角度旋转的应用场合,提出了一种改进的圆投影向量的背景补偿方法。该算法首先利用图像熵自动选择合适的图像参考块,以增强算法的实用性;其次对传统的圆投影向量进行了改进,增加了相位向量以获取背景的旋转参量,并采用核函数定义各像素点的距离权值,从而可以获得更加准确的结果。最后给出了算法步骤,并利用实测数据进行验证。通过仿真实验证明了该算法在各种场景、各种运动情况下的有效性以及对噪声、光照等因素具有鲁棒性。     

无轴承永磁薄片电机转子不平衡振动补偿控制

无轴承永磁薄片电机转子质量的不平衡振动严重影响了系统的动态特性及安全运行。介绍了无轴承永磁薄片电机转子悬浮力产生机理,推导了悬浮转子的动力学方程,在电磁转矩和径向悬浮力解耦控制的基础上,对无轴承永磁薄片电机转子进行了振动补偿控制,设计了反馈不平衡补偿控制系统,采用Matlab/Simulink工具箱构建了仿真系统,进行了性能仿真试验。研究结果表明:基于反馈补偿控制器的振动控制策略能够较好的抑制悬浮转子振动,大大提高了转子的旋转精度。     

Near-optimal cumulative longitude low-thrust orbit transfer

The indirect method for the continuous low-thrust near minimum cumulative longitude orbit transfer problem is addressed. The movement of the satellite is described by the Gauss equation using the modified equinoctial elements and replacing time as the system independent variable by the cumulative longitude. The maximum principle is adapted to design the optimal control in order to minimize the final cumulative longitude, and the twopoint- boundary-value problem is derived from the orbit transfer problem. The single shooting method is applied in a numerical experiment, and the simulations demonstrate that the orbit transfer mission is fulfilled and the product of the maximal thrust and the minimum cumulative longitude is near constant.     

Models of Choosing the Financial Compensation Strategy for Flight Delay

At present, most airlines adopted generally the same amount of compensa- tion strategy when needing to provide financial compensation to all flight delay passengers. However, due to the existence of differences in travel time value, ticket fare, as well as the expectation of compensation for flight delays, the gap between the effect of same amount of compensation and many passengers＇ （especially the high-value ones） expectations is large, it results in that airlines need to pay higher cost of compensation, but the total effect of compensation for passengers are not better. This paper advanced four financial com- pensation strategies for flight delays, summarized their own characteristics, and took into account the interests of both airlines and passengers, built the optimization models of the four financial compensation strategies under the restriction of the airline＇s compensation cost and on the goal of the maximum total effectiveness of the financial compensation to all passengers. Finally, based on the specific circumstances of the flight delays, the paper discussed the method for airline to choose the optimal financial compensation strategy through solving four models and comparing the compensation effectiveness.     

基于快速鲁棒性特征的景象匹配

针对光电成像制导景象匹配中图像产生较大几何形变的问题,提出了一种基于快速鲁棒性特征(speeded up robust feature, SURF)的景象匹配算法。SURF提取的图像特征具有尺度和旋转不变性,对灰度不敏感,并能快速运算。算法首先利用仿射变换对基准图像进行3D视角补偿,模拟基准图像在不同视角下的成像,以减小基准图像和实时图像间的视角差异,分别提取两图像的SURF特征,然后根据最小欧氏距离准则提取两图像间匹配的SURF特征点对,根据该特征点对估计基础矩阵,得到两图像的投影关系。仿真结果表明,该算法能够适应光电成像制导中图像的几何形变,实现稳定的景象匹配。     

相似信息优先的复杂装备费用测算模型

针对横截面数据的复杂装备费用预测问题,由于主要参数比较相似的装备系统其研制费用往往趋同,提出了横截面数据的“相似信息优先原理”。分析新研装备与以往装备的相似度,按照指标信息的相似度区分横截面信息的优先次序。用归一化的相似度作为加权最小二乘法的权重,通过实例建立相似信息优先的回归模型,并与其他方法的结果对比,结果表明本文的方法具有更高的预测精度,相似信息优先的多元回归模型充分反映了相似信息的规律。