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991.
N.M. Polekh K.G. Ratovsky M.G. Deminov O.E. Kolpakova G.P. Kushnarenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Using Irkutsk digisonde data obtained in 2003–2011, a morphological analysis of the G condition occurrence has been made. The G condition was found to occur during daylight hours in summer; in winter, it is extremely rare, and its appearance is associated with intense magnetic storms. In the years of moderate solar activity, the G condition is most frequently registered at Kp ? 4, in the forenoon. During low solar activity, it can be observed under quiet geomagnetic conditions; in most cases, local time of its appearance shifts to afternoon hours. The highest percentage of the G condition occurrence (7.7–6.4%) was recorded in June and July 2008 when the levels of solar and geomagnetic activity were abnormally low. 相似文献
992.
993.
屈建军 《西安航空技术高等专科学校学报》2014,(2):9-11
阶级斗争理论是马克思主义理论的重要组成部分,但这一理论遭到了孙中山的批评。孙中山的批评有错误之处,但谬误中包含着真理。阶级斗争并非历史发展的唯一动力,社会改革也是社会进步的重要途径。 相似文献
994.
分析了民航客机燃油效率的影响因素,将气动阻力进行分解,推导出了以巡航效率为优化目标的最佳机翼优化方法。算例表明,无论是在飞机的方案设计阶段,还是在详细设计阶段,方法都是适用的。方法不仅可用于最佳机翼面积的优化工作,在详细设计阶段,还可用于检验飞机的气动优化设计是否偏离飞机的优化目标,以及检验飞机的最佳巡航航程指标是否与最佳燃油效率匹配。 相似文献
995.
研究了导弹在末制导阶段满足多约束条件下的轨迹优化问题。针对传统方法在处理复杂的非线性运动学、动力学约束上存在的困难,提出了一种基于Radau伪谱方法(RPM)的求解策略。首先,给出了考虑导弹速度和空气密度变化、终端和过程约束条件以及2种不同的性能指标函数的最优轨迹优化问题;其次,利用RPM将轨迹优化问题转化为非线性规划问题,采用序列二次规划算法求得最优解;最后,分2种初始条件对最大落角和最大终端速度的轨迹优化问题进行了仿真验证,结果表明:本文方法能够在较短的时间内生成一条满足多种约束要求的高精度的最优轨迹。 相似文献
996.
《中国航空学报》2016,(2):424-440
The state estimation strategy using the smooth variable structure filter(SVSF) is based on the variable structure and sliding mode concepts. As presented in its standard form with a fixed boundary layer limit, the value of the boundary layer width is not precisely known at each step and may be selected based on a priori knowledge. The boundary layer width reflects the level of uncertainty in the model parameters and disturbance characteristics, where large values of the boundary layer width lead to robustness without optimality and small values of the boundary layer width provide optimality with poor robustness. As a solution and to overcome these limitations, an adaptive smoothing boundary layer is required to achieve greater robustness and suitable accuracy.This adapted value of the boundary layer width is obtained by minimizing the trace of the a posteriori covariance matrix. In this paper, the proposed new approach will be considered as another alternative to the extended Kalman filters(EKF), nonlinear H1 and standard SVSF-based data fusion techniques for the autonomous airborne navigation and self-localization problem. This alternative is based on strapdown inertial navigation system(SINS) and GPS data using the nonlinear SVSF with a covariance derivation and adaptive boundary layer width.Furthermore, the full mathematical model of the SINS/GPS navigation system considering the unmanned aerial vehicle(UAV) position, velocity and Euler angle as well as gyro and accelerometer biases will be used in this paper to estimate the airborne position and velocity with better accuracy. 相似文献
997.
998.
《中国航空学报》2020,33(8):2099-2109
Bent inlet pipes are often used in centrifugal compressors due to limited installation space, and an understanding of the effect on compressor stability is essential for safety and durability. This paper firstly investigates flow instability behaviors in two compressors, one with a straight inlet pipe and the other with an S-shaped bent pipe. In detail, it analyzes the resulting flow fields, instability evolution paths and surge boundaries. The results show that the S-shaped pipe obviously affects the flow field at high mass flow rates, while reverse flow mainly influences the flow field at low mass flow rates. Reverse flow first occurs at certain flow passages with a high pressure difference that is predominantly decided by the volute rather than the S-shaped bent pipe. In addition, centrifugal compressors can tolerate reverse flow to some extent so that surge would not occur immediately if reverse flow occurs unless the reverse flow region extends circumferentially and radially to a sufficiently large size. Since the S-shaped pipe is not dominant in the creation and extension of reverse flow, it does not exacerbate the stability of the central compressor to a great extent. Last but not least, the S-shaped pipe is noted to delay the occurrence of surge at 90% rotating speed, which suggests the possibility of improving compressor stability with bent inlet pipes. This result differs from the conventional understanding that inlet distortion usually deteriorates compressor stability and emphasizes the particularity of centrifugal compressors. 相似文献
999.
1000.
在分析航材消耗件需求规律的基础上,提出了一种基于多元函数的消耗件经济订货批量模型。结合实际数据定义模型参数,利用非线性约束下的广义拉格朗日乘数法即Kuhn-Tucker最优化条件求解模型极值,最终得到基于最佳订货周期和最小费用的最佳订货量。 相似文献