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621.
《中国航空学报》2020,33(2):508-519
A Non-Intrusive Reduced-Order Model (NIROM) based on Proper Orthogonal Decomposition (POD) has been proposed for predicting the flow fields of transonic airfoils with geometry parameters. To provide a better reduced-order subspace to approximate the real flow field, a domain decomposition method has been used to separate the hard-to-predict regions from the full field and POD has been adopted in the regions individually. An Artificial Neural Network (ANN) has replaced the Radial Basis Function (RBF) to interpolate the coefficients of the POD modes, aiming at improving the approximation accuracy of the NIROM for non-samples. When predicting the flow fields of transonic airfoils, the proposed NIROM has demonstrated a high performance. 相似文献
622.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(3):909-932
This paper investigates bottomside thickness parameters at Digisonde stations over midlatitude and high latitude regions, and compares the diurnal, seasonal, and solar activity variations in 2014 and 2009. The geographic latitudes of high latitude considered in this work are located beyond ±60° and those of midlatitude are located between ±40° and ±60°. The IRI-modeled B0 with ABT-2009 option (B0_IRI) are also examined and compared with four kinds of the B0 values, i.e., the observed B0 (B0_obs) from GIRO, the computed B0 following to Jamjareegulgarn et al. (2017a) (B0_old), the calculated B0 with a correction factor regarding to Jamjareegulgarn et al. (2017b) (B0_new), and the B0 with an average correction factor (B0_new_c_av). The average correction factors are proposed additionally in this work so as to assist occasionally the experimental B0 nonexistence of Digisonde which are equal to 0.2658 and 0.2058 for midlatitudes and high latitudes, respectively. Results show that the diurnal variations of B0_new and B0_new_c_av are in a good agreement with those of B0_obs evidently compared with those of B0_IRI and B0_old at every station during the three seasons over high and middle latitudes. During the three seasons, the diurnal variations of B0_new_c_av show similar trends and are close to one another with the B0_obs and the B0_new with small deviations. The differences between the B0obs and the B0_new_c_av also show similar trends and are close to one another with those between the B0obs and the B0_new. In contrast, the B0_IRI with ABT-2009 option seems to predict the B0 values poorly during the three seasons at high latitudes and some seasons at midlatitudes. The proposed B0_new is useful for computing approximately the observed B0 and the ionogram-based total electron content (ITEC) of Digisonde, and the plasma scale height over midlatitudes and high latitudes. 相似文献
623.
Qi Li Jianping Yuan Chong Sun 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(5):1541-1553
In this paper, the motion control problem of autonomous spacecraft rendezvous and docking with a tumbling target in the presence of unknown model parameters, external disturbances, actuator saturation and faults is investigated. Firstly, a nonlinear six degree-of-freedom dynamics model is established to describe the relative motion of the chaser spacecraft with respect to the tumbling target. Subsequently, a robust fault-tolerant saturated control strategy with no precise knowledge of model parameters and external disturbances is proposed by combining the sliding mode control technique with an adaptive methodology. Then, within the Lyapunov framework, it is proved that the designed robust fault-tolerant controller can guarantee the relative position and attitude errors converge into small regions containing the origin. Finally, numerical simulations are performed to demonstrate the effectiveness and robustness of the proposed control strategy. 相似文献
624.
625.
某种叉流板翅式热交换器动态性能的计算 总被引:3,自引:1,他引:2
对某型飞机上应用的一种叉流板翅式热交换器的动态性能进行了计算研究,分别用数值计算方法和参数集中方法进行了计算,给出了计算比较的结果.结果表明,这2种方法计算所得的结果很接近,但是参数集中法计算程序更为简结,适合用于系统模拟的情况. 相似文献
626.
研制出Hopkinson杆(霍普金森杆)高冲击加载装置,搭建起高冲击测试校准系统,基于LabVIEW和Matlab软件开发环境,编写系统控制程序,数据分析与处理程序,以高冲击MEMS加速度传感器为被测对象,开展冲击测试与校准技术研究,解算出传感器冲击灵敏度和频率响应指标。试验结果表明:利用该试验测试装置对冲击传感器进行测试校准,满足传感器主要静态指标测试要求;对传感器频响指标进行测试校准,得到传感器幅频特性和相频特性曲线,满足传感器动态特性测试要求。该Hopkinson杆冲击试验测试校准装置及测控系统能够实现冲击加速度传感器主要静态特性和动态特特指标的测试校准要求,平均灵敏度为0.657 548 μV/g,不确定度优于4%,幅值线性度偏差≤±5%的工作频带为12.5 kHz。本研究对高冲击试验测试的应用提供一定借鉴和参考。 相似文献
627.
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
628.
629.
二级轻气炮是用来模拟空间碎片超高速碰撞效应的重要设备。文章首先介绍了目前二级轻气炮国内外的发展的概况;阐述了其工作原理及所使用的工作气体和试验用品;然后讨论了影响二级轻气炮性能的初始注气压力、活塞速度、弹丸释放压力、活塞质量、弹丸质量等若干参量;最后对反映二级轻气炮性能的重要指标弹丸出口速度和动态碰撞角的测试技术和方法进行了分析。 相似文献
630.