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991.
空客A320飞机横航向控制律采用特征结构配置方法计算闭环增益,实现了期望特征值的配置及横航向关键参数之间的解耦。基于A320横航向控制律架构,提出使用线性二次型(Linear Quadratic,简称LQ)方法,对闭环增益进行重新设计。首先根据期望的特征值引入关键参数的频域整形环节,而后通过调整二次型性能指标加权矩阵实现期望特征值的逼近及关键参数之间的解耦,并求得闭环反馈增益,最后在特征结构、稳定裕度和横航向解耦效果方面与空客设计结果作了对比分析。仿真结果表明,LQ设计可获得与特征结构配置设计相近的结果,即得到接近期望值的特征值,并实现关键变量的解耦,同时保证了闭环稳定裕度。 相似文献
992.
针对采用微小推力进行轨道机动的小卫星,考虑复杂摄动力的基础设计了一种高精度轨道外推和推力在轨标定算法.首先,建立了考虑地球复杂摄动力和微小推力的小卫星轨道动力学模型;然后基于动力学模型,利用变步长龙格库塔算法,设计了对微小推力小卫星进行高精度轨道外推的方法.随后通过无迹卡尔曼滤波器(UKF),设计在轨标定算法,对存在误... 相似文献
993.
994.
Liming He Lixin Wu Sergey Pulinets Shanjun Liu Fan Yang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
A precise determination of ionospheric total electron content (TEC) anomaly variations that are likely associated with large earthquakes as observed by global positioning system (GPS) requires the elimination of the ionospheric effect from irregular solar electromagnetic radiation. In particular, revealing the seismo-ionospheric anomalies when earthquakes occurred during periods of high solar activity is of utmost importance. To overcome this constraint, a multiresolution time series processing technique based on wavelet transform applicable to global ionosphere map (GIM) TEC data was used to remove the nonlinear effect from solar radiation for the earthquake that struck Tohoku, Japan, on 11 March, 2011. As a result, it was found that the extracted TEC have a good correlation with the measured solar extreme ultraviolet flux in 26–34 nm (EUV26–34) and the 10.7 cm solar radio flux (F10.7). After removing the influence of solar radiation origin in GIM TEC, the analysis results show that the TEC around the forthcoming epicenter and its conjugate were significantly enhanced in the afternoon period of 8 March 2011, 3 days before the earthquake. The spatial distributions of the TEC anomalous and extreme enhancements indicate that the earthquake preparation process had brought with a TEC anomaly area of size approximately 1650 and 5700 km in the latitudinal and longitudinal directions, respectively. 相似文献
995.
飞机冲压空气涡轮系统的动态特性分析 总被引:3,自引:0,他引:3
冲压空气涡轮是飞机能源失效时使用的关键应急系统。首先依据冲击空气涡轮(RAT)工作原理确定其物理架构;然后对涡轮部件、能源转换装置、展开装置和展开随动机构等4个主要部件进行力学分析,建立各部件的力学方程组。依据该力学方程组,建立涉及力学、液压、刚体动力学的多学科冲压空气涡轮系统模型。使用该模型仿真了某真实系统在不同工况和设计参数下的动态特性,研究了关键设计参数对系统性能的影响,为冲压空气涡轮系统正向设计提供依据。最终,某型冲压空气涡轮系统风洞试验数据验证了所提系统模型的准确性。 相似文献
996.
受快速傅里叶变换(fast Fourier transform,FFT)的影响,基于FFT和压缩感知(compressive sensing, CS)的脉冲星周期快速估计算法的计算量大。为进一步减小计算量并提高计算精度,利用离散余弦变换(discrete cosine transform,DCT)取代FFT,提出了一种基于DCT-CS的脉冲星周期超快速估计算法。在该方法中,利用DCT提取脉冲星信号的低频部分构建低频DCT矩阵;构建畸变轮廓字典并获取累积轮廓;提出了利用最大值超分辨率稀疏恢复估计脉冲星周期的方法。仿真结果表明,DCT-CS的脉冲星周期估计精度达到了3.82×10-12 s,计算时间达到了9.31 ms。与FFT-CS相比,周期估计精度提高了约16%,计算时间缩短了约37.5%,实现了实时高精度的脉冲星周期估计。 相似文献
997.
998.
Malini Aggarwal H.P. Joshi K.N. Iyer Y.S. Kwak 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
In this paper, response of low latitude ionosphere to a moderate geomagnetic storm of 7–8 May 2005 (SSC: 1920 UT on 7 May with Sym-H minimum, ∼−112 nT around 1600 UT on 8 May) has been investigated using the GPS measurements from a near EIA crest region, Rajkot (Geog. 22.29°N, 70.74°E, Geomag.14°), India. We found a decrease in total electron content (TEC) in 12 h after the onset of the storm, an increase during and after 6 h of Sym-H deep minimum with a decrease below its usual-day level on the second day during the recovery phase of the storm. On 8 May, an increase of TEC is observed after sunset and during post-midnight hours (maximum up to 170%) with the formation of ionospheric plasma bubbles followed by a nearly simultaneous onset of scintillations at L-band frequencies following the time of rapid decrease in Sym-H index (−30 nT/h around 1300 UT). 相似文献
999.
Alexander Tikhomirov Yurii Kudenko Sergey Trifonov Sofya Ushakova 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
The study addresses the possible ways of involving gaseous products produced by “wet” incineration of human wastes mixed with H2O2 in an alternating electric field in the cycling of the physical model of a bio-technical life support system (BTLSS). The resulting gas mixture contains CO2 and O2, which are easily involved in the cycling in the closed ecosystem, and NH3, which is unacceptable in the atmosphere of the BTLSS. NH3 fixation has been proposed, which is followed by nitrification and involvement of the resulting products in the mass exchange of the closed system. Experiments have been performed to show that plants can be grown in the atmosphere resulting from the closing of the gas loop that includes a physicochemical installation and a growth chamber with plants representing the phototrophic compartment of the BTLSS. The results of the study suggest the conclusion that the proposed method of organic waste oxidation can be a useful tool in creating a physical model of a closed-loop integrated BTLSS. 相似文献