飞机突防飞行非线性解耦控制系统的混合仿真研究

飞机低空突防作地形跟踪／回避飞行时，会出现纵向和横向运动的非线性交叉耦合，利用非疆性逆系统理论和现代最优控制理论可以设计一个飞行控制规律来解开这些耦合，主要讨论了这种线性解耦控制系统的混合仿真，给了用于仿真的数学模型以及仿真方法，对系统有无大气紊流扰动的解耦控制、系统对指令输入的跟踪、飞行品质等方面进行了探讨。结果表明，该控制规律在有无大气紊流影响时都能实现解耦，准确地跟踪期望的三维突防航迹，并具     

Time series analysis of active galactic nuclei: The case of Arp 102B, 3C 390.3, NGC 5548 and NGC 4051

We used the Z-transformed Discrete Correlation Function (ZDCF) and the Stochastic Process Estimation for AGN Reverberation (SPEAR) methods for the time series analysis of the continuum and the Hα$\alpha$ and Hβ$\beta$ line fluxes of a sample of well known type 1 active galactic nuclei (AGNs): Arp 102B, 3C 390.3, NGC 5548, and NGC 4051, where the first two objects are showing double-peaked emission line profiles. The aim of this work is to compare the time lag measurements from these two methods, and check if there is a connection with other emission line properties. We found that the obtained time lags from Hβ are larger than those derived from the Hα analysis for Arp 102B, 3C 390.3 and NGC 5548. This may indicate that the Hβ   line originates at larger radii in these objects. Moreover, we found that the ZDCF and SPEAR time lags are highly correlated (r∼0.87$r\sim 0.87$), and that the error ranges of both ZDCF and SPEAR time lags are correlated with the FWHM of used emission lines (r∼0.7$r\sim 0.7$). This increases the uncertainty of the black hole mass estimates using the virial theorem for AGNs with broader lines.     

航天器复杂约束姿态机动的自主规划

 研究了星载设备经受动态环境的多种几何约束和动力学约束时,航天器姿态机动历程的星上规划方法。将完整姿态映射为三维姿态描述空间中的点,姿态路径的规划问题转化为中间节点的规划。随机搜索空间中的一组节点,在相邻节点间采用施加动力学约束的Euler转动姿态制导律,并考查Euler转动过程中的几何约束。用快速搜索随机树方法搜索到可行解,再利用姿态空间特性对路径加以优化。仿真显示算法能在大范围内快速得到可行解,优化措施有助缩短机动时间。离散化的节点规划保证了复杂约束情况下解的有效性,并具有概率完备性。     

Evidence for a Two-Stage Acceleration Process in Large Solar Energetic Particle Events

Using high-resolution mass spectrometers on board the Advanced Composition Explorer (ACE), we surveyed the event-averaged ∼0.1–60 MeV/nuc heavy ion elemental composition in 64 large solar energetic particle (LSEP) events of cycle 23. Our results show the following: (1) The Fe/O ratio decreases with increasing energy up to ∼10 MeV/nuc in ∼92% of the events and up to ∼60 MeV/nuc in ∼64% of the events. (2) The rare isotope ³He is greatly enhanced over the corona or the solar wind values in 46% of the events. (3) The heavy ion abundances are not systematically organized by the ion’s M/Q ratio when compared with the solar wind values. (4) Heavy ion abundances from C–Fe exhibit systematic M/Q-dependent enhancements that are remarkably similar to those seen in ³He-rich SEP events and CME-driven interplanetary (IP) shock events. Taken together, these results confirm the role of shocks in energizing particles up to ∼60 MeV/nuc in the majority of large SEP events of cycle 23, but also show that the seed population is not dominated by ions originating from the ambient corona or the thermal solar wind, as previously believed. Rather, it appears that the source material for CME-associated large SEP events originates predominantly from a suprathermal population with a heavy ion enrichment pattern that is organized according to the ion’s mass-per-charge ratio. These new results indicate that current LSEP models must include the routine production of this dynamic suprathermal seed population as a critical pre-cursor to the CME shock acceleration process.     

Euler computation of the nearfield wake vortex of an aircraft in take-off configuration

Numerical simulations based on the three-dimensional Euler equations are used to investigate the predictive capability of an Euler code for calculations of the nearfield wake of a narrow-body airliner wind tunnel model in take-off configuration up to a half span behind the wing tip trailing edge. Simulation results on both structured and unstructured grids are presented. The results on the block-structured grid were obtained within the scope of the EU-project EUROWAKE. The simulation quality of the vortex formation and spatial development is analysed by comparison to wind tunnel measurements of the spanwise lift distribution available from the EU-project DUPRIN II and to experimental PIV data available from the EU-project EUROWAKE.     

Laser Hardening of Metals

The first experiments on hardening metals by laserpeening induced residual compressive stress in the sur-face of metals for improving their resistance to cracking,stress corrosion and fatigue took place more than 30years ago. However, only today, with the development ofhigh-intensity pulse repetitive rate lasers, this methodstarts to compete to traditional peening, which use influ-ence of small metal balls.Laser peening uses pulses with high intensity 109￣1010 W/cm2 [1]. The laser energy abso…     

Orbital corrections by a single-input impulsive control applied along the geomagnetic field

This paper examines the possibility of regular orbital corrections for a satellite controlled by an impulsive force applied along the induction vector of the local geomagnetic field. The main purpose of the correcting considered in the paper is to eliminate the drift in secular variation of the relative orbital parameters over the orbital period. The obtained results are applied to the formation flying problem. The developed method is tested using numerical simulation.     

太阳耀斑硬X射线高能时延和辐射展宽

本文从耀斑高能电子束流与太阳大气相互作用产生硬X射线辐射的基本事实出发,根据观测资料,提出了一个流量与能谱同步变化的注入源函数模型,研究太阳大气(靶物质)密度对耀斑硬X射线时间响应.理论计算与观测事实基本一致.主要计算结果如下:高能时延与辐射展宽是耀斑硬X射线轫致辐射时间特征的二种表现,硬X射线发射区的太阳大气密度越低,高能时延与辐射展宽效应越明显,二者之间存在显著的相关性.      

KFTA太阳模拟器灯单元的方案设计

在进行KFTA太阳模拟器的设计中,首次采用了氙灯水平点燃的灯单元设计方案。氙灯水平点燃既可以提高太阳模拟器的能量利用率,又降低了成本,节省了人力、物力,但同样也面临着许多新的问题：灯的选择、灯的稳弧、灯的水平调节机构以及灯的应力分析等。文章正是从以上各个方面阐述了KFTA太阳模拟器灯单元的设计思想及方法。     

卫星动不平衡方法研究

文章结合在工程中遇到的动不平衡实际问题,根据平衡机的基本工作原理,提出了双平面分别配重、合成计算的解决思路,并在理论上对自旋稳定卫星的双平面配重的动不平衡配重的计算方法进行了分析和研究,验证了配平计算方法的正确性和可行性。最后,根据配重计算方法提出了配重调整的工艺步骤。