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61.
系统地建立了含湍流的三维低空风切变模型,并综合分析了其对直升机飞行安全的威胁。建立了微下击暴流风场及大气湍流场组合的风切变模型,在不增加计算量的前提下,选取特征点发展直升机飞行动力学模型,有效捕捉了风切变的切变特性,提高了在风场中的动态响应计算精度。模型配备姿态保持功能的控制增稳系统已符合一般直升机的飞行状态,并改善机体响应。根据风速分布的特点,选取不同飞行速度、不同风场位置进行飞行仿真,定性地对比分析状态量变化与风场对应关系,并且以垂向通道为例,从动力学角度分析验证了响应的理论计算表达式。结果表明:湍流主要导致高频姿态角响应,风切变对飞行状态量变化占主导作用,且垂向风是引起威胁的主要因素,据此提出危险风场规避建议。 相似文献
62.
R.V. Garcia P.C.P.M. Pardal H.K. Kuga M.C. Zanardi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(2):1038-1050
This article compares the attitude estimated by nonlinear estimator Cubature Kalman Filter with results obtained by the Extended Kalman Filter and Unscented Kalman Filter. Currently these estimators are the subject of great interest in attitude estimation problems, however, mostly the Extended Kalman Filter has been applied to real problems of this nature. In order to evaluate the behavior of the Extended Kalman Filter, Unscented Kalman Filter and Cubature Kalman Filter algorithms when submitted to realistic situations, this paper uses real data of sensors on-board the CBERS-2 remote sensing satellite (China Brazil Earth Resources Satellite). It is observed that, for the case studied in this article, the filters are very competitive and present advantages and disadvantages that should be dealt with according to the requirements of the problem. 相似文献
63.
Madjid Tavana Faramak Zandi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Sending man to Mars has been a long-held dream of humankind. NASA plans human planetary explorations using approaches that are technically feasible, have reasonable risks and have relatively low costs. This study presents a novel Multi-Attribute Decision Making (MADM) model for evaluating a range of potential mission scenarios for the human exploration of Mars. The three alternatives identified by the Mission Operations Directorate (MOD) at the Johnson Space Center (JSC) include split mission, combo lander and dual scenarios. The proposed framework subsumes the following key methods: first, the conjunction method is used to minimize the number of alternative mission scenarios; second, the Fuzzy Risk Failure Mode and Effects Analysis (RFMEA) is used to analyze the potential failure of the alternative scenarios; third, the fuzzy group Real Option Analysis (ROA) is used to estimate the expected costs and benefits of the alternative scenarios; and fourth, the fuzzy group permutation approach is used to select the optimal mission scenario. We present the results of a case study at NASA’s Johnson Space center to demonstrate: (1) the complexity of mission scenario selection involving subjective and objective judgments provided by multiple space exploration experts; and (2) a systematic and structured method for aggregating quantitative and qualitative data concerning a large number of competing and conflicting mission events. 相似文献
64.
The Coronal Diagnostic Spectrometer (CDS) on SOHO is a grazing/normal incidence spectrograph, aimed to produce stigmatic spectra of selected regions of the solar surface in six spectral windows of the extreme ultraviolet from 150 Å to 785 Å (Harrison et al. 1995). In the present work, CDS, EIT, MDI and Yohkoh observations of active region lops have been analyzed. These observations are part of JOP 54. CDS monochromatic images from lines at different temperatures have been co-aligned with EIT and MDI images, and loop structures have been clearly identified using Fe XVI emission lines. Density sensitive lines and lines from adjacent stages of ionization of Fe ions have been used to measure electron density and temperature along the loop length; these measurements have been used to determine the electron pressure along the loop and test the constant pressure assumption commonly used in loop modeling. The observations have been compared with a static, isobaric loop model (Landini and Monsignori Fossi 1975) assuming a temperature-constant heating function in the energy balance equation. Good agreement is found for the temperature distribution along the loop at the coronal level. The model pressure is somewhat higher than obtained from density sensitive line ratios. 相似文献
65.
Ion-induced nucleation has been suggested to be a potentially important mechanism for atmospheric aerosol formation. Ions
are formed in the background atmosphere by galactic cosmic rays. A possible connection between galactic cosmic rays and cloudiness
has been However, the predictions of current atmospheric nucleation models are highly uncertain because the models are usually
based on the liquid drop model that estimates cluster thermodynamics based on bulk properties (e.g., liquid drop density and
surface tension). Sulfuric acid (H2SO4) and water are assumed to be the most important nucleating agents in the free troposphere. Measurements of the molecular
thermodynamics for the growth and evaporation of cluster ions containing H2SO4 and H2O were performed using a temperature-controlled laminar flow reactor coupled to a linear quadrupole mass spectrometer as well
as a temperature-controlled ion trap mass spectrometer. The measurements were complemented by quantum chemical calculations
of the cluster ion structures. The analysis yielded a complete set of H2SO4 and H2O binding thermodynamics extending from molecular cluster ions to the bulk, based on experimental thermodynamics for the small
clusters. The data were incorporated into a kinetic aerosol model to yield quantitative predictions of the rate of ion-induced
nucleation for atmospheric conditions. The model predicts that the negative ion-H2SO4-H2O nucleation mechanism is an efficient source of new particles in the middle and upper troposphere. 相似文献
66.
以大型液体火箭发动机故障诊断系统框架为基础,按照发动机不同工作阶段的特点建立了相应的故障检测与诊断算法。利用发动机的高队数学模型,对基于推广的卡尔曼滤波器技术的新息检测算法进行了研究。根据发动机系统工作过程的特点,建立了降阶故障模式响应模型,并发展了相应的故障模式检验方法。为了适应在线实时检测的需要,利用发动机的试验数据,分别研究了基于人工神经元网络辨识模型的发动机启动过程检测算法和基于时间序列分析方法的发动机主机工作过程检测算法。通过试验数据的检测验证,证明了这些实时算法的快速性、准确性和鲁律性。 相似文献
67.
损耗大气中随机重力波场的传输方程 总被引:3,自引:0,他引:3
从包含分子粘性的非线性相互作用方程出发, 采用随机相位近似, 推导了损耗大气中重力波场的非线性传输方程。由于分子损耗的引入, 谱演变的速率发生了改变, 在某些情况下, 还会得到与无耗条件下的传输规律相反的结论。损耗大气中重力波场的传输方程是研究中高层大气重力波能量收支平衡的出发点。 相似文献
68.
简述控制高层大气的主要能源和描绘了高层大气的主要天气变化过程,并且阐明高层大气及其预报研究的量要性和给出高层大气对航天飞行有严重影响的几个实例,最后简介高层大气及其预报研究的新动向。 相似文献
69.
70.
木星探测是未来行星探测的重要发展方向,而降落伞是进入木星大气探测必不可少的气动减速装置。文章基于“伽利略号”探测任务,设计了满足未来木星探测需求的降落伞系统简化模型,并针对该降落伞系统进行了数值模拟,研究了木星大气和地球风洞实验环境中不同来流马赫数下降落伞系统的复杂流动现象及气动力变化规律。在木星大气环境中,降落伞的阻力系数和横向力系数大小以及横向力系数波动幅度均高于风洞试验环境,阻力系数波动幅度均低于风洞实验环境。此外,还研究了木星大气环境中不同来流攻角下降落伞系统的气动特性。研究表明,木星大气环境中降落伞系统气动特性与风洞实验结果有差异,因此未来在设计用于木星探测的降落伞系统时,应考虑由于木星大气环境对降落伞系统气动特性的影响。 相似文献