利用PB 6.0实现数据库动态查询

在分析关系数据库SQL查询语言原理的基础上,通过一个具体的例子介绍了如何利用PB6.0实现数据库动态查询.     

圆柱壳承受水下爆炸作用时的动响应

本文提出了有限水域内水下爆炸实验设计的一般考虑方法,结合实验结果得到了各种条件(λ/D)下圆柱壳受水下爆炸作用时的壁压分布规律,采用塑性动力学中绝对最小原理对结构响应进行了数值计算,给出了冲击波作用下圆柱壳响应的一种偏安全估算方法。     

核动力装置主系统对蒸汽发生器给水流量的动态响应

本文把集总参数法用于堆芯、一回路和二回路,导出了主系统对蒸汽发生器给水流量丧失的动态方程组及其解析解,非常适用于运行监督性快速计算。     

Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface

Based on fuzzy adaptive and dynamic surface (FADS), an integrated guidance and control (IGC) approach was proposed for large caliber naval gun guided projectile, which was robust to target maneuver, canard dynamic characteristics, and multiple constraints, such as impact angle, limited measurement of line of sight (LOS) angle rate and nonlinear saturation of canard deflection. Initially, a strict feedback cascade model of IGC in longitudinal plane was established, and extended state observer (ESO) was designed to estimate LOS angle rate and uncertain disturbances with unknown boundary inside and outside of system, including aerodynamic parameters perturbation, target maneuver and model errors. Secondly, aiming at zeroing LOS angle tracking error and LOS angle rate in finite time, a nonsingular terminal sliding mode (NTSM) was designed with adaptive exponential reaching law. Furthermore, combining with dynamic surface, which prevented the complex differential of virtual control laws, the fuzzy adaptive systems were designed to approximate observation errors of uncertain disturbances and to reduce chatter of control law. Finally, the adaptive Nussbaum gain function was introduced to compensate nonlinear saturation of canard deflection. The LOS angle tracking error and LOS angle rate were convergent in finite time and whole system states were uniform ultimately bounded, rigorously proven by Lyapunov stability theory. Hardware-in-the-loop simulation (HILS) and digital simulation experiments both showed FADS provided guided projectile with good guidance performance while striking targets with different maneuvering forms.     

控制力矩陀螺的动态扫描成像卫星姿态控制

针对卫星动态扫描成像任务中的姿态控制问题,建立卫星姿态动力学模型,分析动态扫描成像任务对姿态控制的特殊需求。结合动态扫描成像任务需求提出一种典型的姿态机动方案,对姿态机动过程所需控制力矩进行估计。基于期望力矩和星体实时姿态设计一种俯仰机动控制律,并提出五棱锥构型陀螺群的操纵方案。针对某动态扫描成像任务卫星,对提出的控制律进行数值仿真。仿真结果证明所提方案可以满足卫星动态扫描成像的姿态控制要求。     

船用蒸汽发生器的动态模型与模拟研究

以船舶核动力装置中广泛使用的立式U形管自然循环蒸汽发生器为对象,从其热工水力特点分析出发,建立蒸汽发生器的动态模型,并对其运行模拟及应用进行了研究。     

The timing of contests

We develop a simple model to analyze the timing of contests. When the odds of winning a contest are exogenously given – we show that if either the players discount the future or if the total cost of contest is smaller in the future – there exist subgame perfect equilibria where both players settle, anticipating a contest in the future. With endogenous efforts, the aggregate efforts expanded in a contest are smaller if the contest occurs in the future when the relative effort productivities remain constant or diverge over time, thus creating scope for delay in contests. When the effort productivities converge over time, the total efforts may be greater under a future contest. As a consequence, players either settle over the two periods, or else they initiate a contest immediately.     

The military as a learning organisation: establishing the fundamentals of best-practice in lessons-learned

The post-Cold War era has witnessed the rapid expansion of organisational learning initiatives within NATO militaries, especially formal “lessons-learned” processes. The effectiveness of national lessons-learned processes in recalibrating military activity to the demands of ongoing operations has been highly-differentiated. However, the academic literature on military change and practitioner guidance has been slow to investigate the key features of best-practice in military learning. This article breaks new ground by drawing upon the literature on dynamic organisational capabilities to explore the fundamental organisational processes and activities which are necessary to implement successful lessons-learned. It examines, in particular, the organisational features which facilitate “knowledge transformation”: the effective combination of new knowledge gained from intra- and inter-organisational learning with existing organisational knowledge. The article concludes by highlighting several potential future empirical and theoretical research agendas in military learning and the importance of engagement between lessons-learned practitioners and organisational learning scholars.     

火星稀薄大气动态误差对制动降轨的影响

针对火星大气制动降轨过程中稀薄流区大气受季节和昼夜等因素影响而存在较大动态误差的问题,建立气动力作用下的轨道动力学方程,研究探测器稀薄流气动参数计算方法,分析大气参数动态误差对气动力及制动降轨效果的影响。结合火星探测应用,仿真分析火星大气制动过程中的探测器气动特性以及轨道变化特性。为保证探测器制动过程中的安全和持续时间要求,给出了理想的大气制动降轨走廊范围及导航精度需求,具有一定的工程参考价值。     

用弹性动力学基本分析方法求解导弹 折叠翼展开的动响应

用机构弹性动力学的基本方法分析了一种导弹折叠翼展开的动力学问题,详细介绍了运动微分方程的解法,并将计算结果曲线与刚体动力学计算曲线、试验测得的曲线进行比较和分析,证明了该算法的可靠性和可行性。