Recovering of the thermal band of Landsat 7 SLC-off ETM+ image using CBERS as auxiliary data

The failure of scan-line corrector (SLC-off) has resulted in the limited use of Landsat 7 ETM+ images. Considering its characteristics, many attempts have been conducted to recover the SLC-off ETM+ image. While much attention has been paid to recovering the optically multispectral bands, few researches have been done to reconstruct the thermal band. Main purposes of our study were to evaluate the possibility that using China Brazil Earth Resources Satellite (CBERS) as auxiliary data to recover the thermal band of SLC-off ETM+, and discuss the usage of the recovered one. The adaptive window linear histogram match (AWLHM) method was selected primarily, followed by the modified one. Results illustrated the feasibility of using the modified AWLHM method with the linear combination of CBERS-01 band3 and band4 to reconstruct the SLC-off thermal band. It encourages that further researches should be done to enable more scientific application of SLC-off ETM+, particularly its’ thermal band.     

Morphological and molecular changes of maize plants after seeds been flown on recoverablf satellite

Dry seeds of Zea mays, heterozygous for Lw₁/lw₁ alleles, sandwiched between nuclear track detectors aboard Chinese satellite for 15 days, were recovered and mutations in morphological characters on plants developed from these seeds, as well as their selected progenies, were investigated. The dosimetric results indicated that 85% of the seeds received at least 1 hit with Z≥20. About 10% of plants developed from flown seeds and 40% of observed selfed lines from the first generation plants showed some morphological changes, such as yellow stripes displayed on leaves, dwarf, anomogensis of floral organs and yellow-green seedlings, when compared with those from ground control. Using yellow stripes on leaves as the main endpoint for evaluating mutation induced in space environment, the frequency of stripe occurrence was 4.6% in the first generation plants, comparable with the results obtained from Long Duration Exposure Facility (LDEF) mission (Mei et al., 1994), but much lower than those from ground based ⁶⁰ Co-gamma treatment at a dose of 100 Gy, which reached 35.5% in the selfed lines of the second generation. One hundred and ten random primers were screened in RAPD analysis to detect the variation on genomic DNA of plants with stripes on leaves. Of these primers, 10.9% were able to generate polymorphic bands between mutated plants and control, also, common band patterns in several progenies with the same mutation phenotype were observed. These results demonstrated that space radiation environment could induce inheritable mutagenic effects on plant seeds, and verified the change in genetic material in the mutants. Further study will be needed for a better understand of the nature and mechanism of this induction of mutation.     

机载公共设备综合管理系统任务分配算法研究

机载公共设备的综合管理是机载系统发展的必然方向,为解决机载公共设备综合管理系统中任务分配问题,进行了任务划分.根据周期任务和非周期任务对系统风险系数的贡献不同,提出了两层任务分配策略;以单机风险系数均衡为目标函数,设计了基于蚁群算法的周期任务分配算法.对蚁群算法进行了模糊自适应参数调整的改进,仿真结果表明改进算法能够有效地使蚁群算法从局部最优点中逃脱,解决任务分配问题.      

翼型气动性能鲁棒性优化设计

讨论了一种在来流速度不确定的情况下对翼型进行鲁棒性设计的方法.介绍了单点及多点设计方法后,阐述了鲁棒性设计方法在翼型气动性能优化中的应用,并对三者进行了比较.引入了代理模型以减少计算量, 并通过遗传算法对翼型进行鲁棒性设计.借助区间分析方法讨论了翼型设计变量的扰动对气动特性上下界值的影响.应用该方法,在提高了翼型的气动性能的同时,降低了该性能对于来流速度的敏感度.      

基于模糊奇偶方程的PL/INS导航系统故障诊断

提出了一种伪卫星(PL, Pseudolite)/惯性导航(INS, Inertial Navigation System)组合导航系统多故障识别方法.分析了PL的常见故障及其数学模型,采用模糊奇偶方程方法对PL的常见故障进行诊断、隔离和参数识别.采用Takagi-Sugeno(T-S)模糊模型描述PL/INS组合导航系统,对于局部线性化模型建立全解耦奇偶方程,并对奇偶方程的残差进行融合,得到全局残差.结合残差利用卡尔曼滤波进行故障参数识别,给出了参数识别的约束条件.仿真结果表明:针对导航系统中多个PL信号同时发生多种故障的情况,此方法能有效检测故障,并能准确识别出故障模型参数.      

机器人在卫星舱板装配中的应用研究

因卫星部分外舱板上需要安装有效载荷,而载荷与卫星主结构之间有多束电缆连接。舱板的安装通常需要使用翻转工装,为了保证舱板的安装精度,在装配过程中要求多名装配工人相互配合才能完成。文章对目前卫星舱板装配过程进行了分析,结合舱板安装实际,提出了机器人辅助自动化装配、半自动化装配方案及其运动路径基本算法。方案的实现有助于推动卫星自动化装配的进程,并提高装配工作效率。     

刚体航天器姿态跟踪的时变滑模控制(英文)

To solve the problem of attitude tracking of a rigid spacecraft with an either known or measurable desired attitude trajectory, three types of time-varying sliding mode controls are introduced under consideration of control input constraints. The sliding surfaces of the three types initially pass arbitrary initial values of the system, and then shift or rotate to reach predetermined ones. This way, the system trajectories are always on the sliding surfaces, and the system work is guaranteed to have robustness against parameter uncertainty and external disturbances all the time. The controller parameters are optimized by means of genetic algorithm to minimize the index consisting of the weighted index of squared error （ISE） of the system and the weighted penalty term of violation of control input constraint. The stability is verified with Lyapunov method. Compared with the conventional sliding mode control, simulation results show the proposed algorithm having better robustness against inertia matrix uncertainty and external disturbance torques.     

结构静力响应区间的一种计算方法及工程应用

针对实际工程中广泛存在的物理或几何上的不确定性,提出一种有界不确定性结构静力响应上下确界的有效计算方法,将线形区间方程组转化为两个标准的线性规划问题求解,并给出数学证明.编写与大型有限元软件ANSYS的接口程序和区间运算程序,使区间运算方法和工程有限元软件结合并推广到实际工程领域.以某大跨钢结构建筑为例,对其静力响应区间进行估计.结果表明,该方法可给出与Deif方法一致的精确结果且计算量较之Deif方法大幅降低.基于此算法对ANSYS进行二次开发的接口程序和区间运算程序,可直接用于含有界不确定性参数的实际工程问题中.      

伴飞航天器轨道修正点状态的最小二乘估计

研究了近圆轨道航天器长期伴随飞行在轨道修正时刻相对状态的最小二乘估计方法。针对长期伴飞航天器在固定时刻进行轨道修正的特点,提出采用最小二乘估计方法对轨道修正时刻的相对位置状态进行估计,并基于模型误差特点提出对该算法进行改进的加权最小二乘估计算法。算法具有计算相对简单、算法灵活等特点。仿真结果表明,对于固定时刻的状态估计,这种加权最小二乘估计算法和扩展卡尔曼滤波算法的效果相当,能够满足在轨长期伴随飞行在轨道修正时刻的相对状态估计精度要求。     

返回式航天器轨道周期变率确定及预报的数值方法

对返回式航天器进行变轨控制计算时要用到平均轨道周期变率,而数值法定轨通常求解的是大气阻力系数,无法直接得到平均轨道周期变率。文章通过建立航天器精密动力学模型、数值积分器、瞬时轨道根数到平均轨道根数的转换算法和平均周期序列多项式拟合算法,提出了一种基于数值法精密轨道确定和预报计算平均轨道周期变率的数值方法。