基于落点预测的高旋火箭弹弹道修正算法

高旋火箭弹的修正控制是基于等效力实现的二维弹道修正控制，由于弹体存在陀螺进动和马格努斯效应，在控制力作用下产生的附加攻角引起的升力与控制力的矢量合为等效力，其大小与方向在控制过程中不断变化，不能简单根据偏差量（修正量）的比例关系来确定控制力的方向。基于此，分析了控制力与等效力的关系，提出了一种基于弹道落点预测的控制算法。首先利用弹道落点预测模型实时预测落点与目标的偏差量，然后利用小扰动法构造偏差量对控制量的敏感系数矩阵，通过偏差量与敏感系数矩阵解算出纵、横两个方向的需用控制量。采用修正前后速度矢量的位置关系得到控制量的合矢量及其方位角，并利用控制量的合矢量与等效力计算出控制周期，在控制周期内按照等效力方位角调整控制力的方向实现对高旋火箭弹的精确控制，解决了非线性耦合问题。仿真结果表明该算法具有较高的控制精度，为工程应用提供理论依据。     

我国计量行业法规政策和发展趋势分析

计量是实现单位统一、保证量值准确可靠的活动，关系国家安全、国计民生。为夯实计量基础、提升计量能力，抓住计量事业发展的新机遇，本文从行业法规政策、计量发展趋势等方面开展相关研究，为从事计量管理和技术研究工作的人员提供参考。     

Attitude stability and periodic attitudes of rigid spacecrafts on the stationary orbits around asteroid 216 Kleopatra

In this work, equilibrium attitude configurations, attitude stability and periodic attitude families are investigated for rigid spacecrafts moving on stationary orbits around asteroid 216 Kleopatra. The polyhedral approach is adopted to formulate the equations of rotational motion. In this dynamical model, six equilibrium attitude configurations with non-zero Euler angles are identified for a spacecraft moving on each stationary orbit. Then the linearized equations of attitude motion at equilibrium attitudes are derived. Based on the linear system, the necessary conditions of stability of equilibrium attitudes are provided, and stability domains on the spacecraft’s characteristic plane are obtained. It is found that the stability domains are distributed in the first and third quadrants of the characteristic plane and the stability domain in the third quadrant is separated into two regions by an unstable belt. Subsequently, we present the linear solution around a stable equilibrium attitude point, indicating that there are three types of elemental periodic attitudes. By means of numerical approaches, three fundamental families of periodic solutions are determined in the full attitude model.     

EW射频隐身系统频率选择表面电磁散射参数的测量

频率选择表面(FSS)技术为电子战射频隐身提供了新的实现技术途径,散射参数的测量验证是射频隐身系统FSS设计的关键环节.针对非理想测量环境,以一种小型化带阻频率选择表面为例,提出了一套频率选择表面散射参数的测量和校准方法,有效消除了测量中信号的衰减、测量天线间的耦合以及信号多径传播等对真实结果造成的影响,使之尽可能接近在理想环境中的测试结果.该方法极大改善了周期性人工电磁结构散射参数测量对环境的依赖,降低了射频隐身FSS设计的研发成本,在电子战领域具有良好的应用前景.     

Postcapture stabilization of space robots considering actuator failures with bounded torques

Space robotics is regarded as one of the most impressing approaches for space debris removal missions. Due to the residual momentum of debris, it is essential to stabilize the base rapidly after capture. This paper presents a novel control strategy for stabilization of a space robot in postcapture considering actuator failures and bounded torques. In the control strategy, the motion of the manipulator is not regarded as a disturbance to the base; in contrast, it is utilized to compensate for the limitation of the control torques by means of an inverse dynamical model of the system. Different scenarios where actuators are external mechanisms or momentum exchange devices have been carried out, and for actuator failures, both single- and two-actuator failures have been considered. Regarding to the performance of actuators, control torques are bounded. In cases that either single or two actuators have failed, the base can be stabilized kinematically when actuators are external mechanisms, but can only be stabilized dynamically when only momentum exchange devices are used. Finally, a space robot with a seven-degree-of-freedom manipulator in postcapture is studied to verify the validity and feasibility of the proposed control scheme. Simulation results show that the whole system can be stabilized rapidly.     

除冰液对道面混凝土的影响及保护剂防护效果

通过冻融和化学侵蚀试验，研究了NW-056A机场道面除冰液对道面水混混凝土耐久性的影响以及在道面除冰液环境下两种新型混凝土保护剂的防护效果。结果表明：①混凝土在道面除冰液中冻融后表面无明显剥落现象，相对动弹模损失率比在水中小很多，道面除冰液延缓了混凝土的冻融破坏：②混凝土在道面除冰液常温浸泡下表面无剥蚀现象，但强度比在水中降低很多，因此存在化学腐蚀．且主要表现为对混凝土内部结构的缓慢损伤；（④两种新型混凝土保护剂均对预防混凝土的冻融破坏以及除冰液环境下的腐蚀破坏起到一定作用，涂刷混凝土保护剂是提高混凝土道面耐久性的有效方法。     

系留气球囊体外形优化研究

利用基于约束的Kanikdale修正算法,以及一套用于确定尾翼尺寸和系留缆绳外形的方法,并借助基于GA的GADO优化器,对系留气球囊体形状进行了优化研究。结果表明,通过多材料组合方式生成的囊体,其有效载重能力能够提升6.5%左右。     

面向PLM的协同工艺设计与管理技术研究与应用

结合对某航空制造企业工艺设计业务流程的分析,以CAPPFramework与Teamcenter集成开发为基础,建立了由数据层、协同平台层、应用层构成的协同工艺设计与管理系统(C-CAPP)架构,详细论述了主制工艺与协作工序/扩编工艺的编制协同,主制工艺编制与专用工装申请/设计的协同,主制工艺与数控加工工序的编制协同,工艺设计数据管理方式。并以XML为工具进行了C-CAPP系统功能调用和数据通信形式化描述。     

Study on dependence of hydrodynamic characteristics on gravity in a vertical upward channel bubbly flow

Since the bubbly flow has extensive applications in the space field, it is very necessary to comprehend the dependence of hydrodynamic characteristics on gravity. In this paper, the dependence of the microbubble distribution and the liquid turbulence modulation by the microbubbles on gravity was investigated in detail with the Euler–Lagrange method. The liquid Navier–Stokes equation was solved using direct numerical simulations (DNS), and the microbubble motion was tracked with Newtonian motion equation considering drag force, shear lift force, added mass force, pressure gradient force, and wall lift force. The coupling between the gas and the liquid phases regarded the interphase force as a momentum source term in the momentum equation of the liquid. The results showed that the phase profile and the turbulence modulation by the microbubbles strongly depend on the magnitude of gravity. When the influence of gravity is relatively weak, the microbubbles approximately uniformly disperse in the wide central region of the channel, and the average statistics of the liquid turbulence are almost not influenced due to the addition of the microbubbles. However, when the influence of gravity is comparatively important, the majority of the microbubbles accumulate near the wall of the channel, and the injection of the microbubbles modifies the profiles of the liquid average statistics.