Mechanistic identification of cutting force coefficients in bull-nose milling process

An improved method to determine cutting force coefficients for bull-nose cutters is proposed based on the semi-mechanistic cutting force model. Due to variations of cutting speed along the tool axis in bull-nose milling, they affect coefficients significantly and may bring remarkable discrepancies in the prediction of cutting forces. Firstly, the bull-nose cutter is regarded as a finite number of axial discs piled up along the tool axis, and the rigid cutting force model is exerted. Then through discretization along cutting edges, the cutting force related to each element is recalculated, which equals to differential force value between the current and previous elements. In addition, coefficient identification adopts the cubic polynomial fitting method with the slice elevation as its horizontal axis. By calculating relations of cutting speed and cutting depth, the influences of speed variations on cutting force can be derived. Thereby, several tests are conducted to calibrate the coefficients using the improved method, which are applied to later force predictions. Eventually, experimental evaluations are discussed to verify the effectiveness. Compared to the conventional method, the results are more accurate and show satisfactory consistency with the simulations. For further applications, the method is instructive to predict the cutting forces in bull-nose milling with lead or tilt angles and can be extended to the selection of cutting parameters.     

An experimental study of the dual-loop control of electro-hydraulic load simulator （EHLS）

This paper investigates motion coupling disturbance（the so called surplus torque）in the hardware-in-the-loop（HIL）experiments.The＇＇velocity synchronization scheme＇＇was proposed by Jiao for an electro-hydraulic load simulator（EHLS）in 2004.In some situations,however,the scheme is limited in the implementation for certain reasons,as is the case when the actuator＇s valve signal is not available or it is seriously polluted by noise.To solve these problems,a＇＇dual-loop scheme＇＇is developed for EHLS.The dual-loop scheme is a combination of a torque loop and a position synchronization loop.The role of the position synchronization loop is to decouple the motion disturbance caused by the actuator system.To verify the feasibility and effectiveness of the proposed scheme,extensive simulations are performed using AMESim.Then,the performance of the developed method is validated by experiments.     

Evaluation of COMPASS ionospheric model in GNSS positioning

As important products of GNSS navigation message, ionospheric delay model parameters are broadcasted for single-frequency users to improve their positioning accuracy. GPS provides daily Klobuchar ionospheric model parameters based on geomagnetic reference frame, while the regional satellite navigation system of China’s COMPASS broadcasts an eight-parameter ionospheric model, COMPASS Ionospheric Model(CIM), which was generated by processing data from continuous monitoring stations, with updating the parameters every 2 h. To evaluate its performance, CIM predictions are compared to ionospheric delay measurements, along with GPS positioning accuracy comparisons. Real observed data analysis indicates that CIM provides higher correction precision in middle-latitude regions, but relatively lower correction precision for low-latitude regions where the ionosphere has much higher variability. CIM errors for some users show a common bias for in-coming COMPASS signals from different satellites, and hence ionospheric model errors are somehow translated into the receivers’ clock error estimation. In addition, the CIM from the China regional monitoring network are further evaluated for global ionospheric corrections. Results show that in the Northern Hemisphere areas including Asia, Europe and North America, the three-dimensional positioning accuracy using the CIM for ionospheric delay corrections is improved by 7.8%–35.3% when compared to GPS single-frequency positioning ionospheric delay corrections using the Klobuchar model. However, the positioning accuracy in the Southern Hemisphere is degraded due apparently to the lack of monitoring stations there.     

喷泉码在遥测应用中的误码扩散研究

喷泉码是一种近年来发展起来的适用于删除信道的纠删码技术,可用于恢复传输过程中丢失的数据。在火箭、导弹遥测信道下,不仅存在由于信号闪断而丢失数据的现象,而且存在由随机噪声引起的误码。若误码符号进入喷泉码译码器,则会引起严重的误码扩散现象。提出一种以喷泉码为外码、信道纠错码为内码的级联方案,并采用误码消除技术克服误码扩散问题,从而解决恶劣信道环境下(噪声信道+闪断信道)的数据传输问题。     

对星载滑动聚束模式合成孔径雷达的侦察研究

滑动聚束模式是合成孔径雷达的一种新兴的工作模式,具有比条带模式的方位向分辨率高、同时又比聚束模式的成像区域大的优点,因此,滑动聚束模式呈现蓬勃发展的趋势。在此基础上,根据侦察的基本原理,展开了对滑动聚束模式合成孔径雷达的侦察研究,建立了侦察模型,并进行了仿真实验。可以看出,对星载滑动聚束模式合成孔径雷达的侦察是完全可行的。     

Trajectory tracking control for underactuated stratospheric airship

Stratospheric airship is a new kind of aerospace system which has attracted worldwide developing interests for its broad application prospects. Based on the trajectory linearization control (TLC) theory, a novel trajectory tracking control method for an underactuated stratospheric airship is presented in this paper. Firstly, the TLC theory is described sketchily, and the dynamic model of the stratospheric airship is introduced with kinematics and dynamics equations. Then, the trajectory tracking control strategy is deduced in detail. The designed control system possesses a cascaded structure which consists of desired attitude calculation, position control loop and attitude control loop. Two sub-loops are designed for the position and attitude control loops, respectively, including the kinematics control loop and dynamics control loop. Stability analysis shows that the controlled closed-loop system is exponentially stable. Finally, simulation results for the stratospheric airship to track typical trajectories are illustrated to verify effectiveness of the proposed approach.     

基于IVI驱动的真空热试验数据采集系统软件开发

目前国内大型空间环境模拟器配备了多种型号的数据采集系统,主要负责完成对多种数据信号的综合测试。文章以Keithley 3706数据采集系统为设计对象,在VB6.0的开发环境中设计了基于IVI驱动的数据采集软件,给出了IVI驱动的设计过程及软件代码。实践表明,IVI驱动的引入提高了数据采集系统的开发效率,降低了研制成本,实现了数据采集系统的硬件无关性。     

航天器真空热试验人员窒息预想事故的事故树分析

事故树分析法具有逻辑性强、形象化的特点,将安全事故与原因用逻辑树图的方式表现出来,能够系统分析安全事故产生的原因,明确安全管理工作的重点。文章对航天器真空热试验人员窒息预想事故进行了事故树分析,分析了导致事故发生的基本事件,求取了最小割集、最小径集,并对基本事件进行了结构重要度分析,根据分析结果提出了安全预防措施的建议。     

基于全脉冲的周期信号样本提取技术

现代电子战中,传统的辐射源分选识别方法无法在密集的信号环境中快速有效地对复杂体制雷达进行分选识别,造成系统漏警。基于上述情况,提出了一种基于脉冲样本序列自提取的分选算法。这种算法利用雷达信号脉冲序列的周期性和相关性,实现对模板序列的自动提取,从而可实现全脉冲序列中小样本数或脉间规律复杂的雷达信号的分选。仿真实验表明,在全脉冲数据量级适中的情况下,该算法可以有效提取目标模板序列。     

鲁棒的结构网格自动化重叠方法

网格技术是目前数值模拟中的关键技术之一。重叠网格是一种放宽拓扑要求、减小网格生成难度的网格技术。本文以结构重叠网格为基础,分别针对挖洞、寻点以及洞面优化方法进行了研究和改进,同时完成物面网格重叠,形成了一套鲁棒的、自动化的网格重叠系统。在挖洞方面,结合“最小洞映射”方法,提出“复合式挖洞”方法,节省内存开销;在寻点方面,通过构建格心虚网格,保证搜索空间的连续性,同时结合“有效搜索”思想,排除部分对寻点无贡献的网格点,进而减少ADT叉树节点;在洞面优化上,改变填补判别法则并引入两类受保护洞内点,确保两层插值边界建立,提高鲁棒性;在物面网格重叠上,利用物面投影法完成坐标修正,实现物面附近网格流动变量的准确传递。为验证本文方法,分别对定常翼身组合体DLR-F6绕流和非定常机翼挂载分离过程进行了数值模拟,计算结果与实验结果吻合良好,表明该结构重叠网格系统对多物体间定常、非定常扰流具有较好的数值模拟能力和较高的模拟精度,具有较高的工程应用价值。