带有状态滞后的连续广义系统的鲁棒正实控制﹡

对带有状态滞后的连续广义系统的严格正实性进行了分析,得出了这类系统渐近稳定且严格正实的充分条件,该充分条件与滞后无关。进一步地,对这类系统带有不确定性和控制量的情况进行了研究。提出了一种基于线性状态反馈控制的鲁棒正实控制器设计方法,使得控制器设计可以通过求解线性矩阵不等式方便地加以解决,且保证了闭环系统的严格正实性。最后,通过实例分析说明所提出的鲁棒正实控制器设计方法是可行的、有效的。     

略论《文子》"以正治国,以奇用兵"用兵思想及其进步性

作为先秦道家重要典籍,传世本《文子》第十二篇《上礼》继承了老子“以正治国,以奇用兵”的思想。其“以正治国”强调随时、顺性、合俗、利民、能因、无为,在此基础上,其“以奇用兵”强调因民之欲、不从己出、用兵以诚、用兵以时、以仁用兵、用兵以礼、用兵以道等。与诸子相比,具有独特之处。这在1978年河北定县汉墓出土的竹简《文子》残文中得到证明。本文试从分析《文子》“以正治国,以奇用兵”内涵入手,来探讨《文子》用兵思想的特点。     

战争宣传演进的历史考察

宣传与战争相伴而生,战争宣传的发展与人类战争形态的演变息息相关。从冷兵器战争、热兵器战争、机械化战争到信息化战争形态,战争宣传手段由简单到复杂,战争宣传形式由单一到多样,战争宣传的地位由辅助到独立。从人类战争形态演变的视角全面考察战争宣传的历史演进,有助于深刻认识战争宣传的内涵和全貌,全面加强信息化条件下的军事宣传工作。     

坚持用科学发展观指导空军转型建设

坚持用科学发展观指导空军转型建设,必须牢牢把握“发展”这一主题,用新的发展思路实现空军更快更好发展;深入贯彻“统筹兼顾,协调发展”的方针,走出一条中国特色空军发展之路;始终坚持“以人为本”这个核心,以人才转型为先导带动空军转型建设全面发展。     

随移动窗推进的带电粒子束团长程传输模拟分析

直接采用粒子模拟方法较难实现带电粒子束团千米量级的长程传输模拟,针对此问题以静电模型为基础,引入移动窗技术,使百米量级的粒子传输窗口与束团同步推进运动,建立了带电粒子束团的长程传输模型。将模拟得到的带电粒子束团径向膨胀特性同包络方程的计算结果进行对比,两者吻合较好,证明了在带电粒子束团长程传输模拟研究中结合移动窗技术的可行性及所建模型的合理性。利用此模型分析了100 MeV相对论电子束团的长程传输过程,发现传输过程中束团的自生电场和磁场在径向上呈高度对称分布,轴向上则呈轻微前冲分布;同时,束团内部粒子的轴向速度分布也会发生变化。利用此模型分析了100 MeV电子束团的长程传输过程及其内部参数和自生场量的变化。     

Simulation of the plasticizing behavior of composite modified double-base (CMDB) propellant in grooved calendar based on adaptive grid technology

The frequent occurrence of safety accidents during the calendering process is caused by the flammable and explosive properties of composite modified double-base (CMDB) propellant. Optimization of process parameters with the aid of fluid simulation technology could effectively ensure the safety of the calendering process. To improve the accuracy of the simulation results, material parameters and model structure were corrected based on actual conditions, and adaptive grid technology was applied in the local mesh refinement. In addition, the rheological behavior, motion trajectories and heat transfer mechanisms of CMDB propellant slurry were studied with different gaps, rotational rates and temperatures of two rollers. The results indicated that the refined mesh could significantly improve the contour clarity of boundaries and simulate the characteristics of CMDB propellant slurry reflux movement caused by the convergent flow near the outlet. Compared with the gap, the increased rotational rate of roller could promote the reflux movement and intensify the shear flow of slurry inside the flow region by viscous shear dragging. Meanwhile, under the synergistic effect of contact heat transfer as well as convective heat exchange, heat accumulated near the outlet and diffused along the reflux movement, which led to the countercurrent heat dissipation behavior of CMDB propellant slurry. The plasticizing mechanism of slurry and the safety of calendering under different conditions were explored, which provided theoretical guidance and reference data for the optimization of calendering process conditions. Based on the simulation results, the safety of the CMDB propellant calendering process could be significantly improved with a few tests conducted during a short research and development cycle.     

Polarization visualization for low-irradiance regions by perceptually uniform color space

Currently,polarization visualization strategies are accomplished by mapping polarization information into a perceptually uniform color appearance model CAM02-UCS.However,the deviation of the CAM02-UCS space from the lightness prediction results in an inaccurate match between the polarization in-formation and the perceptual information.In this paper,we propose a novel polarization visualization strategy based on the perceptual uniform space Jzazbz.The polarization visualization be completed by placing the polarization information into the lightness Jz,colorfulness Cz and hue angle hz channels of the Jzazbz space.The experimental results show that the proposed method can significantly improve the lightness of the low irradiance and high polarization region,hence more polarization information can be sensed by human visual system.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.     

飞船再入制导最佳反馈增益系数规律

为了获取基于标准轨道返回舱再入纵向制导的最佳反馈增益系数 ,建立了纵平面运动方程 ,推导了对应于纵向制导规律的摄动微分方程。根据Pontryagin极小值原理 ,给出了最优反馈控制律 ,求解Riccati方程 ,即可得到最佳反馈增益系数。考虑到实现的可行性 ,将时变的增益系数逼近成常数或分段常数 ,得到次优反馈增益系数 ,取得了满意的制导效果。     

惯性导航系统故障诊断的不确定性问题研究

针对构造惯性导航系统 ( INS)故障诊断所面临的确定性和不确定性问题 ,提出了基于模糊集理论的诊断方法 ,并给出诊断系统自动获取不确定性证据和确定性证据隶属度的方法及函数 .认为对于确定性证据和不确定性证据可以用统一的方法和原则来处理 ,并建立了两类证据的实用数学模型