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161.
对航天器结构进行频率匹配设计,是降低耦合响应,控制其在发射阶段动力响应水平的有效方法,文章进行了局部系统动力特性的频率匹配技术研究。用基于响应谱分析的频率匹配技术优化配置局部系统的固有频率,使其与整星动力学特性和动态激励特性更加匹配,并结合结构动力特性优化使局部系统频率满足设计值。通过工程实例,验证了该方法用于控制航天器动力响应的有效性,优化后设备加速度响应幅值相对于优化前降低了20%~40%。 相似文献
162.
Alessandro Settimi Marco Pietrella Michael Pezzopane Bruno Zolesi Cesidio Bianchi Carlo Scotto 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The present paper proposes to discuss the ionospheric absorption, assuming a quasi-flat layered ionospheric medium, with small horizontal gradients. A recent complex eikonal model (Settimi et al., 2013b) is applied, useful to calculate the absorption due to the ionospheric D-layer, which can be approximately characterized by a linearized analytical profile of complex refractive index, covering a short range of heights between h1 = 50 km and h2 = 90 km. Moreover, Settimi et al. (2013c) have already compared the complex eikonal model for the D-layer with the analytical Chapman’s profile of ionospheric electron density; the corresponding absorption coefficient is more accurate than Rawer’s theory (1976) in the range of middle critical frequencies. Finally, in this paper, the simple complex eikonal equations, in quasi-longitudinal (QL) approximation, for calculating the non-deviative absorption coefficient due to the propagation across the D-layer are encoded into a so called COMPLEIK (COMPLex EIKonal) subroutine of the IONORT (IONOspheric Ray-Tracing) program ( Azzarone et al., 2012). The IONORT program, which simulates the three-dimensional (3-D) ray-tracing for high frequencies (HF) waves in the ionosphere, runs on the assimilative ISP (IRI-SIRMUP-P) discrete model over the Mediterranean area ( Pezzopane et al., 2011). As main outcome of the paper, the simple COMPLEIK algorithm is compared to the more elaborate semi-empirical ICEPAC formula (Stewart, undated), which refers to various phenomenological parameters such as the critical frequency of E-layer. COMPLEIK is reliable just like the ICEPAC, with the advantage of being implemented more directly. Indeed, the complex eikonal model depends just on some parameters of the electron density profile, which are numerically calculable, such as the maximum height. 相似文献
163.
《中国航空学报》2021,34(2):466-478
With the development of Unmanned Aerial Vehicle (UAV) system autonomy, network communication technology and group intelligence theory, mission execution in the form of a UAV swarm will be an important realization of future applications. Traditional single-UAV mission reliability modeling methods have been unable to meet the requirements of UAV swarm mission reliability modeling. Therefore, the UAV swarm mission reliability modeling and evaluation method is proposed. First, aimed at the interdependence among the multiple layers, a multi-layer network model of a UAV swarm is established. At the same time, based on the system having the following characteristics—using a mission chain to complete the mission and applying the connectivity of the mission network—the mission network model of a UAV swarm is established. Second, vulnerability and connectivity are selected as two indicators to reflect the reliability of the mission, and aimed at random attack and deliberate attack, vulnerability and connectivity evaluation methods are proposed. Finally, the validity and accuracy of the constructed model are verified through simulations, and the model and selected indicators can meet the reliability requirements of the UAV swarm mission. In this way, this study provides quantitative reference for UAV-swarm-related decision-making work and supports the development of UAV-swarm-related work. 相似文献
164.
The Chinese air transport system has witnessed an important evolution in the last dec-ade, with a strong increase in the number of flights operated and a consequent reduction of their punctuality. In this contribution, we propose modelling the process of delay propagation by using complex networks, in which nodes are associated to airports, and links between pairs of them are assigned when a delay propagation is detected. Delay time series are analysed through the well-known Granger Causality, which allows detecting if one time series is causing the dynamics observed in a second one. Results indicate that delays are mostly propagated from small and regio-nal airports, and through flights operated by turbo-prop aircraft. These insights can be used to design strategies for delay propagation dampening, as for instance by including small airports into the system's Collaborative Decision Making. 相似文献
165.
为了修正舰船运动和海风引起的落点误差,首先建立了雷伞系统各阶段动力学模型并进行了编程计算,通过与试验结果的对比验证了动力学模型的准确性。之后,将发射方向和分离时间作为控制量,基于泰勒级数理论推导了落点误差与控制量之间的关系,提出了一种新的雷伞系统落点误差的修正方法。通过算例验证,该方法所得到的控制参数能够有效地修正雷伞系统的落点误差。同时,针对典型工况开展了本文方法与改进的多目标粒子群轨迹优化算法的对比研究,发现本文方法比改进的多目标粒子群优化算法拥有更快的收敛速度、更高的收敛精度和更少的计算消耗,可以对由舰船运动和海风引起的雷伞系统落点误差进行实时准确地修正,从而提高舰船发射布雷的精度。 相似文献
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169.
针对无线通讯系统和雷达系统的数字仿真中大量存在的复包络数字滤波器建模问题 ,提出了一种基于变量误差模型 (Errors- in- Variables Model,简记为 EV模型 )的频域最大似然参数估计方法。首先将实验测量值的中心频率移到零频 ,得到复包络滤波器的频率响应 ,然后使用最小二乘法计算复包络滤波器系数的初始估计值 ,最后使用数值迭代法对最大似然估计的代价函数进行优化 ,得到复包络滤波器系数的最佳估计。实验结果以及理论分析表明 ,与现有的复包络数字滤波器转换方法相比 ,最大似然法建模的过程更加直接 ,结果更加精确 相似文献
170.
角形结构的电磁散射和雷达截面分析 总被引:6,自引:0,他引:6
角形结构是飞行器及其它许多目标的强散射源之一。本文采用复射线展开法分析了双平面角形结构的雷达截面,所得计算结果与实验结果及其它方法的理论结果十分吻合。 相似文献