飞行器切换多胞系统抗干扰控制

针对存在参数不确定和外部扰动的飞行器切换多胞系统跟踪控制问题,提出了一种基于改进微分器的抗干扰控制方法。该方法将参数不确定和外部扰动带来的影响均视为干扰,提出一种改进微分器实现对干扰的精确光滑估计并设计控制器进行补偿,抑制干扰对系统的影响。与H∞等传统鲁棒方法相比,本文所提方法避免了对不确定满足凸包形式的假设,且在名义情况和不确定情况下均具有良好的性能。结合微分不等式理论和平均驻留时间方法证明了闭环系统的稳定性。为了验证本文所提方法的良好性能,将其应用到一类高超声速飞行器的轨迹跟踪控制问题中,仿真结果表明该方法能够有效抑制干扰,实现对参考信号的精确跟踪。     

基于速度增量修正的卫星入轨段外测数据定轨新方法

在传统的数值积分精密定轨方法基础上,提出基于器箭分离速度增量修正的定轨方法,实现了器箭分离前后两段外测数据的联合定轨。仿真计算结果和任务实战数据验证结果表明,该方法大大提高了地月转移轨道入轨段外测定轨精度,比传统初轨确定方法提高约一个数量级。     

系留悬浮式风力发电技术的研究进展与展望

风力发电作为清洁能源利用的重要方式,具有无污染、可再生、方便采集等特点,近年来得到快速发展。相对于传统低空风力发电,系留悬浮式风力发电具有容量系数高、发电成本低等优点,拥有更大的开发价值和发展潜力,已有多个国家开展研究并取得一定成果。本文通过对系留悬浮式风力发电技术发展的调研,归纳四种系留悬浮式风力发电技术类型,分析各技术类型的工作原理与特点,总结未来系留悬浮式风力发电需要重点突破的轻质高强系留缆绳设计与制造、高性能囊体复合材料、稳定与智能控制、高效风力发电飞行平台总体设计、便利展开部署五种关键技术,为后续研究提供参考。     

基于先前CPI多维数据的天基雷达信号处理算法

为了消除单站天基雷达非稳态杂波图景的影响,讨论一种利用先前CPI（Coherent Processi     

Simulations of the microwave sky and of its “observations”

Here follows a preliminary report on the construction of fake millimeter and sub-millimeter skies, as observed by virtual instruments,e.g. the COBRA/SAMBA mission, using theoretical modeling and data extrapolations. Our goal is to create maps as realistic as possible of the relavant physical contributions which may contribute to the detected signals. This astrophysical modeling is followed by simulations of the measurement process itself by a given instrumental configuration. This will enable a precise determination of what can and cannot be achieved with a particular experimental configuration, and provide a feedback on how to improve the overall design. It is a key step on the way to define procedures for the separation of the different physical processes in the future observed maps. Note that this tool will also prove useful in preparing and analyzing current (e.g. balloon borne) Microwave Background experiments.     

CME dynamics using coronagraph and interplanetary ejecta data

In this work, we present a study of the coronal mass ejection (CME) dynamics using LASCO coronagraph observations combined with in-situ ACE plasma and magnetic field data, covering a continuous period of time from January 1997 to April 2001, complemented by few extreme events observed in 2001 and 2003. We show, for the first time, that the CME expansion speed correlates very well with the travel time to 1 AU of the interplanetary ejecta (or ICMEs) associated with the CMEs, as well as with their preceding shocks. The events analyzed in this work are a subset of the events studied in Schwenn et al. (2005), from which only the CMEs associated with interplanetary ejecta (ICMEs) were selected. Three models to predict CME travel time to Earth, two proposed by Gopalswamy et al. (2001) and one by Schwenn et al. (2005), were used to characterize the dynamical behavior of this set of events. Extreme events occurred in 2001 and 2003 were used to test the prediction capability of the models regarding CMEs with very high LASCO C3 speeds.