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881.
本文讨论了数字余度飞行控制系统中的几个主要问题。根据随机过程假设提出了一种故障监控门限值的选取方法:余度管理软件的分时多速率结构,以及基于卡尔曼滤波器的解析余度方案。另外,本文还提出了伺服器均衡回路的独立性概念,从而解决了均衡回路的设计问题。 相似文献
882.
近室温磁制冷工质选择的热力学准则 总被引:7,自引:0,他引:7
对近年来在制冷界研究相当活跃的磁制冷的工质,尤其是近室温磁制冷的工质-铁磁材料,在外加磁场中的热力学特性进行了分析、讨论,并在此基础上总结了选取近室温磁制冷工质的理论依据和原则,使实际中的选择工作有了针对性,减少了盲目性。 相似文献
883.
运用流体动力学分析,指出了涡轮流量计的Thompson—Grey理论模型中存在的各种缺陷。计算结果表明,改进后的模型与实际情况的吻合程度有了很大提高,涡轮流量计仪表系数的理论估计值与实际值之间的偏差由原来的±(4%~6%)下降至±1.5%以内。 相似文献
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888.
分析了通过窄缝隙耦俣的矩形波导H面T形接头对(以下简称HT对)的电气特性,利用等效原理和切向场连续性建立积分方程组,采用矩量法化积分方程为代数方程进行数值求解,获得散射场和等效散射参数,以X波段标准矩形波导HT接头对为例进行具体求解和计算,以及实验验证,得到良好结果。 相似文献
889.
The best active twist schedules exploiting various waveform types are sought taking advantage of the global search algorithm for the reduction of hub vibration and/or power required of a rotor in high-speed conditions.The active twist schedules include two non-harmonic inputs formed based on segmented step functions as well as the simple harmonic waveform input.An advanced Particle Swarm assisted Genetic Algorithm (PSGA) is employed for the optimizer.A rotorcraft Computational Structural Dynamics (CSD) code CAMRAD Ⅱ is used to perform the rotor aeromechanics analysis.A Computation Fluid Dynamics (CFD) code is coupled with CSD for verification and some physical insights.The PSGA optimization results are verified against the parameter sweep study performed using the harmonic actuation.The optimum twist schedules according to the performance and/or vibration reduction strategy are obtained and their optimization gains are compared between the actuation cases.A two-phase non-harmonic actuation schedule demonstrates the best outcome in decreasing the power required while a four-phase non-harmonic schedule results in the best vibration reduction as well as the simultaneous reductions in the power required and vibration.The mechanism of reduction to the performance gains is identified illustrating the section airloads,angle-of-attack distribution,and elastic twist deformation predicted by the present approaches. 相似文献
890.
Gang Hai Huan Xie Wenjia Du Menglian Xia Xiaohua Tong Rongxing Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(7):2120-2139
Slope correction is important to improve the accuracy of satellite radar elevation measurements by mitigating the slope-induced error (SE), especially over uneven ground surfaces. Although several slope correction methods have been proposed, guidance in the form of stepwise algorithm on how to implement these methods in processing radar altimetric data at the coding level, and the differences among these methods need to be presented and discussed systematically. In this paper, three existing types of slope correction methods—the direct method (DM), intermediate method (IM), and relocation method (RM, further divided into RM1 and RM2)—are described in detail. In addition, their main differences and features for various scientific applications are analyzed. We conduct a systematic experiment with CryoSat-2 Low Resolution Mode (LRM) data in a physically stable area around Dome Argus in East Antarctica, where in-situ measurements were available for comparison. The slope correction is implemented separately using the three methods, with the latest high-accuracy Reference Elevation Model of Antarctica (REMA) as the a-priori topography model. The bias and precision of the slope-corrected CryoSat-2 data results from the RM2 is ?0.18 ± 0.86 m based on the comparison with the field Global Navigation Satellite System (GNSS) data. The results from the RM2 indicate higher precision compared to those from the RM1. According to the correlation analysis of the slope-corrected CryoSat-2 data results (RM1 and RM2), the bias enlarges and the precision becomes worse when the surface slope increases from 0 to 0.85°. After a comprehensively comparative analysis, we find that the results from the RM1 and RM2 are superior in precision (0.93 m and 0.86 m) with respect to the GNSS data. The relatively low precision (1.22 m) from the IM is due to the potential error from the a-priori digital elevation model (DEM). The DM has the lowest precision (2.66 m). Another experiment over rough topography in West Antarctica is carried out for comparison, especially between the RM1 (precision of 15.27 m) and RM2 (precision of 16.25 m). In general, the RM is recommended for the SE elimination among the three methods. Moreover, the RM2 is firstly considered over smooth topography due to the superior performance in bias and precision, while the RM1 is more suggested over the rough topography because of the slightly smaller bias and better precision. The IM relies much on the accuracy of the a-prior DEM and is not usually recommended, because of the strict requirement in the sampling time between the radar altimetry data and the a-priori DEM to avoid any surface change over time. 相似文献