Adaptive predefined-time control for liquid-filled flexible spacecraft attitude stabilization during orbit maneuver

A predefined-time attitude stabilization for complex structure spacecraft with liquid sloshing and flexible vibration is investigated under input saturation during orbital maneuver. First, the attitude dynamics model of liquid-filled flexible spacecraft is constructed. Meanwhile, the influence of solar panel vibration and liquid sloshing is treated as a disturbance in the controller design. Next, an adaptive predefined-time control scheme is proposed by applying sliding mode control theory. A predefined-time convergent sliding surface and reaching law are designed to ensure the predefined-time fast convergence rate. Furthermore, a novel adaptive algorithm is developed to handle the disturbances from liquid sloshing and flexible vibration, ensuring that the system converges to a small neighborhood of the equilibrium. Additionally, a new auxiliary system is constructed to deal with the effects of input saturation. At last, one simulation case is performed to verify the feasibility and advantages of the proposed algorithm.     

中国电视节目生产的本土化策略

研究中国电视节目生产中实施"本土化"策略的方式和意义。从电视媒体的生存环境入手,结合跨国媒体集团以及国内几家电视台本土化策略成功运用的案例,进行系统综合分析。使人们对电视节目的"本土化"有一个比较客观、理性的认识。那些能体现本土特色的电视节目才真正具有市场竞争力,才能吸引观众的眼球。     

Effect of surface roughness on microwave brightness temperature from lunar surface: Numerical analysis with a hybrid method

A hybrid method, combining the radiative transfer theory and the method of moments (MoM), is proposed to study the potential effect of the lunar surface roughness on the microwave brightness temperature. The total upward emission reaching the lunar surface from below media is calculated by the radiative transfer theory, and then the brightness temperature is obtained by weighting the bidirectional transmission coefficients which is computed using the MoM. The method is validated by both flat and rough surface models with analytic solutions. With the hybrid method, brightness temperatures from simulated lunar model are calculated and compared to those from a flat layered model. The comparisons show that the effect of rough surface on brightness temperature cannot be ignored and also depends on many other factors, such as observation angle and polarizations. For vertical polarization, an optimal observation angle may exist to reduce the effect of surface roughness. These results indicate that the knowledge of lunar surface roughness is important in microwave remote sensing to the Moon and may probably provide a guide to lunar projects in future.     

《热工学》精品课程建设研究

精品课程建设是体现试点专业特色的标志之一.在对《热工学》精品课程的建设思路、建设项目、及建设方法分析和探讨基础上,提出了笔者的一些体会,以达到与同行相互交流的目的.     

推力室参数对喷管化学动力学性能的影响

针对某液体发动机进行化学动力学计算，研究了各种推力室参数，如燃烧室压强、混合比、边区冷却流量以及喷管的尺寸等对喷管性能的影响。由计算结果可以得到参数变化引起性能变化的定量的规律，分析推力室设计的优劣，提出改善发动机性能的具体措施。     

几种液体火箭发动机喷注器的研制

介绍了几种液体火箭发动机喷注喷研制中出现的技术问题及其解决途径。同时,对双组元离心式喷嘴流量偏差作了分析,探讨了控制流量偏差的方法。提出的一种身部内冷却装置,采用斜齿缝隙钎焊整体式结构,在中等推力液体火箭发动机中进行试验得出初步结论。     

三组元推进剂燃烧试验分析

三组元火箭发动机是近几年提出的新概念.本文介绍了三组元推进剂燃烧试验及其结果分析.试验用液氧/丙烷/氢做推进剂在9.78MPa燃烧室压力下完成.试验结果表明,三组元推进剂和三组元发动机概念可行.     

液晶瞬态技术测量带侧向流扰流柱通道端壁换热

采用热色液晶瞬态测量技术测量带侧向流扰流柱通道端壁全表面换热系数的分布,研究了侧流比及雷诺数对换热的影响,其中,侧流比为0.25~1.0,雷诺数为3×104~9×104。结果表明:(1)侧流比对扰流柱通道的流动形态及端壁换热有重要影响;(2)存在一个临界侧流比,在临界侧流比以下,流动形态沿主流方向呈错排流状态;在临界侧流比以上,流动形态沿侧流方向呈错排流状态;在临界侧流比附近,流动为顺排流动状态,方向在主流和侧流方向之间;(3)侧流比较小或较大时,扰流柱通道端壁换热较强;在临界侧流比附近,换热相对较弱。     

国外空间液体剩余量测量技术

掌握卫星运行期间剩余推进剂的贮量是掌握卫星活动的重要一环。为了精确测量空间液体，欧空局推出两种测量方法──定期容量激励法和外来质量注入法。介绍了这两种空间液体测量方法；描述了Ｇ－２２搭载实验；给出了实验结果。     

二次启动前火箭发动机泵构件温度特性数值计算

用数值计算的方法研究了液体火箭发动机在二次启动前，发动机泵系统各构件的温度特性和泵腔含汽率。建立了基于集总参数法的发动机启动前排放过程中涡轮、泵及进口管的温度变化计算模型。排放冷却过程中冷却剂N2O4的单相强制对流换热系数用Dittus-Boelter公式计算，流动沸腾换热系数采用Shan M M强化模型。并对某液体火箭发动机二次启动前排放过程涡轮泵系统各构件温度变化和泵腔含汽率进行了计算，模型计算结果与试车数据吻合良好，研究结果表明，二次启动前的主动排放过程对泵壳体及进口管的冷却效果很好。