关于“质量问题归零”前移的探讨

结合QQJA10-2002《航天产品质量问题归零实施要求》,探讨了航天产品质量问题归零工作前移的路子,阐述了质量问题归零工作前移的目的、意义、可行性、实施方式和效果评价,并对开展质量问题归零工作前移的相关要求、实施可能遇到的问题及对策进行了分析和说明。     

动力学反演的迭代过程及应用

把结构动力学反演归结为一类广义特征值反问题 ,提出了一种迭代算法 ,并讨论了解的存在条件。大量数值实验结果表明 ,本文迭代过程收敛性好。结合某型直升机旋翼桨叶的动力学设计 ,文中给出了工程应用的数值例子 ,结果令人满意。     

关于提高集团公司资金管理水平的探讨

随着市场经济的发展,跨地区甚至跨国的集团化公司大量涌现,而集团公司在经营拓展的同时没有强化对资金的管理,造成集团公司在资金管理方面中出现了诸多问题.要解决这些问题,必须强化资金管理,建立以财务资金管理为核心的内部信息管理系统,运用现代信用工具实行资金集中收付,通过全面预算管理、内部审计等手段有效监控使用资金,保证资金的合理有效使用,提高资金管理水平.     

加强设计文件的标准化审查

介绍了设计文件标准化审查的目的及主要内容,分析了存在的问题,对设计文件标准化审查中常见的错误作了说明,并提出了采取的措施。     

金融衍生工具会计问题探讨

金融衍生工具具有衍生性、杠杆性、创新性和风险转移性等特点, 这些特点对现有会计理论产生着极大的冲击,影响着会计要素的确认、计量和披露,并且冲击着传统损益的确认.     

大数据时代下的思维变革、问题与应对决策

随着互联网技术的不断更新、数据信息的急剧增长,大数据时代已被开启。为了更好地顺应这次重大的时代转型,文章从大数据的基本含义、时代特征入手,引出大数据时代下,爆炸性的数据是如何变革着我们的思维方式,同时指出了大数据时代下面临的问题,分享了应对决策,以期提高社会对大数据的关注度和适应能力。     

DSMC热化学模拟分子数对氮氧离解反应计算影响的分析

准确模拟高速流场中的热化学非平衡问题一直都是各种流场数值计算的难点。DSMC作为一种有效的流场模拟方法,从统计学的角度而言,作为统计母体的模拟分子数是影响计算准确性的关键。Bird等[Bird,1990]针对不涉及热化学非平衡的流场提出了一个统一的模拟分子数选取规则。本文在热浴条件下使用DSMC模拟了空气中三种常见氮氧气体的离解反应,对涉及热化学非平衡的流场中模拟分子数对DSMC精度的影响进行了分析。结果表明:与Bird针对普通流场所提出的统一模拟分子数选取规则不同,在不同的流场物理条件(本文主要为温度)下,得到正确结果的模拟分子数阈值与温度成正相关(最小离解度与最大离解度模拟分子数选择下限相差10倍),超出阈值后增加模拟分子数对流场精度并无明显提高,这一结果与Parker的分子能量传递理论相符。从保证计算精度和平衡计算效率的角度,本文的结论对DSMC非平衡流场模拟具有参考价值。     

Robust fault detection and optimization for a network of unmanned vehicles with imperfect communication channels

The observer-based robust fault detection and optimization for a network of unmanned vehicles with imperfect communication channels and norm bounded modeling uncertainties are addressed. The network of unmanned vehicles is modeled as a discrete-time uncertain Markovian jump system. Based on the model, a residual generator is constructed and the sufficient condition for the existence of the desired fault detection filter is derived in terms of linear matrix inequality. Furthermore, a time domain optimization approach is proposed to improve the performance of the fault detection system. The problem of detecting small faults can be formulated as an optimization problem and its solution is given. For preventing false alarms, a new adaptive threshold function is established. The combined fault detection and optimization algorithm and the adaptive threshold are then applied to a network of highly maneuverable technology vehicles to illustrate the effective- ness of the orooosed aooroach.     

Attitude synchronization for multiple spacecraft with input constraints

The attitude synchronization problem for multiple spacecraft with input constraints is investigated in this paper. Two distributed control laws are presented and analyzed. First, by intro- ducing bounded function, a distributed asymptotically stable control law is proposed. Such a con- trol scheme can guarantee attitude synchronization and the control inputs of each spacecraft can be a priori bounded regardless of the number of its neighbors. Then, based on graph theory, homoge- neous method, and Lyapunov stability theory, a distributed finite-time control law is designed. Rig- orous proof shows that attitude synchronization of multiple spacecraft can be achieved in finite time, and the control scheme satisfies input saturation requirement. Finally, numerical simulations are presented to demonstrate the effectiveness and feasibility of the oroDosed schemes.