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111.
配置压电自感作动器复合层板的振动主动控制 总被引:2,自引:1,他引:1
采用一阶剪应变理论,对具有自感作动器的复合层板进行有限元分析,为避免自由度数太大,采用按结构模态展开的方法,给出以模态坐标为变量的状态方程,和以电流为输出的观测方程。在此基础上,考虑振动系统的外激励干扰衰减 LQG,H∞ 控制问题。对具有四对压电薄膜的层板结构进行了数值仿真,绘制出LQG控制下和 H∞ 控制下闭环系统控制对象的奇异值曲线,还给出持续外力作用下速度响应曲线比较,仿真结果表明控制的方法是有效的。 相似文献
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113.
魏屹 《长沙航空职业技术学院学报》2008,8(2):68-70
运用安全管理的一般原理,从现阶段我国企业安全管理的现状着手,分析和提出企业安全管理中普遍存在的问题,重点研究产生问题的原因,并在此基础上,系统论述解决问题的对策与建议。 相似文献
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115.
李园庭 《南昌航空工业学院学报》2007,21(4):8-12
讨论了一类拟线性椭圆型方程的CHOQUARD-PEKAR问题在无界区域中的非平凡解的存在性,对于极小问题Iλ和I∞λ,得到了对于每个λ0,存在α∈(0,λ],使得Iα和I∞α可以达到. 相似文献
116.
针对拥有共享内存的并行计算环境和微机网络并行计算环境,给出了求解大型稀疏对称矩阵部分极端特征对的并行块Davidson方法。该方法将矩阵A按行块分配到各处理器上,各处理器利用矩阵A的行块和投影子空间的正交基所组成矩阵V的行块进行运算,减少了处理机之间的通讯次数,实现了算法的并行计算。在微机网络并行计算环境和拥有共享内存并行计算环境IBMP650上的数值试验表明,该算法非常有效。 相似文献
117.
《中国航空学报》2021,34(2):252-264
The technique of imaging a target with a complicated motion using an Inverse Synthetic Aperture Radar (ISAR) system is an effective tool in the field of radar signal processing. After the translational compensation, the received signal reflected from the target can take the form of a multi-component Polynomial Phase Signal (m-PPS), and the high quality ISAR image can be provided via the combination between the estimated parameters of the m-PPS and the Range Instantaneous-Doppler technique (RID). For a target with a high maneuvrability, the occurrence of scatterers Migration Through Resolution Cell (MTRC), caused by the rotational movement could be appearing. That is why the variation in the amplitude of the echo during the time of observation cannot be neglected. The purpose of this study is the parameters estimation of the m-PPS signal with order three in the case of the Time Varying Amplitude (TVA). The Improved-version of the Product High-order Ambiguity Function (IPHAF) with TVA is proposed to improve the quality of the ISAR image compared with traditional techniques based on a constant amplitude; the experimental outcomes confirm that the new IPHAF-TVA method presented in this study is an effective technique to make the ISAR image very clear. 相似文献
118.
针对现有地外天体软着陆安全着陆点选择方法的不足,设计了逆金字塔式安全着陆点选择方法,结合着陆器的落点精度和自主避障及地形坡度适应能力,建立了基于平整点、安全着陆点、可靠避障点和标称着陆点的地形安全性分析与定量搜索模型,该模型呈四层逆金字塔结构,每一层搜索的结果作为下一层搜索的输入,从弱约束到强约束逐步收敛至100%地形安全着陆区,嫦娥五号探测器飞行结果表明该方法能够快速确定安全着陆区及标称着陆点,并有效指导着陆下降过程的标称航迹设计和轨道控制策略制定。 相似文献
119.
Andrea D’Ambrosio Dario Spiller Fabio Curti 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(11):3462-3477
The development of fast and reliable optimization algorithms is required in order to obtain real-time optimal trajectory on-board spacecraft. In addition, the wide spread of small satellites, due to their low costs, is leading to a greater number of satellite formations in space. This paper presents an Improved version of the Magnetic Charged System Search (IMCSS) metaheuristic algorithm to compute time-suboptimal manoeuvres for satellite formation flying. The proposed algorithm exploits some strategies aimed at improving the convergence to the optimum, such as the chaotic local search and the boundary handling technique, and it is able to self-tune its internal parameters and coefficients. Moreover, the inverse dynamics technique and the differential flatness approach, through the B-splines curves, are used to approximate the trajectory. The optimization procedure is applied to the circular J2 relative model developed by Schweighart and Sedwick and to the elliptical relative motion model developed by Yamanaka and Ankersen. The results of this paper show that the convergence is better achieved by using the proposed tools, thus proving the efficiency and reliability of the algorithm in solving some space engineering problems. 相似文献
120.
Wafaa Kanaan David Farrelly Víctor Lanchares 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(8):2124-2134
A restricted 2?+?2 body problem is proposed as a possible mechanism to explain the capture of small bodies by a planet. In particular, we consider two primaries revolving in a circular mutual orbit and two small bodies of equal mass, neither of which affects the motion of the primaries. If the small bodies are temporarily captured in the Hill sphere of the smaller primary, they may get close enough to each other to exchange energy in such a way that one of them becomes permanently captured. Numerical simulations show that capture is possible for both prograde and retrograde orbits. 相似文献