文化反哺：大学生过度社会化与辅导员嵌入性行为研究

社会文化变迁将会更新社会文化的内容体系,影响社会文化的传承方式。当今社会中80后、90后大学生已经出现了社会化程度过高或社会化速度加快的趋势,过度社会化导致在大学生群体中出现与其年龄阶段不符的思想与行为,影响了大学生社会化的顺利开展,不利于高校思想政治教育的顺利开展。本文以文化反哺现象为视角,探讨在大学生过度社会化进程中辅导员的嵌入性行为模式,以期为新时期高校思想政治教育改革与发展提供新思路。     

高超声速飞行器自抗扰分数阶PID控制器设计(英文)

自抗扰控制器利用跟踪微分器可解决超调量及快速性之间的矛盾,分数阶PID控制器在提高控制品质的同时扩大了被控系统参数的稳定域。结合自抗扰技术及分数阶PID控制器设计了自抗扰分数阶PID控制器,并应用于高超声速飞行器再入姿态控制。仿真结果表明,自抗扰分数阶PID控制器对于高超声速飞行器非线性模型及强外干扰的影响下具有很好的控制效果,并且有较大的稳定域,即针对被控系统参数变化具有更强的鲁棒性。     

光纤陀螺开环增益的实时估计与补偿

开环增益是影响闭环光纤陀螺控制稳定性及控制精度的重要参数。从光纤陀螺的数学模型出发推导了开环增益的计算公式。在数字闭环光纤陀螺相关检测的基础上提出了一种开环增益的估计方法,通过在积分控制环节前施加一个方波抖动信号,然后在信号处理器中进行相关解调,实现了开环增益的在线实时估计。同时利用数字逻辑中比例控制系数的可操作性,通过实时调整比例控制系数K来补偿硬件部分增益G的变化,从而实现陀螺开环增益的自补偿。最后通过实验证明了该方法的正确性。     

一个面向可变形模型实时有效的接触反馈框架

由于力反馈需要很高的计算速度及变形反馈需要详细的图形信息 ,本文提供一个实时有效的接触反馈框架 ,通过在粗糙三角形网格上进行局部细分来实现。当检测到接触后 ,将发生碰撞的表面细分以产生一个粒子系统。利用此粒子系统 ,用近似速度锥理论对形变进行模拟。同时 ,采用弹簧 -阻尼模型计算形变力。最后 ,对此框架进行了测试并实际应用于一个医疗规化仿真系统。     

免疫反馈算法及其在航空发动机控制中的应用

基于生物免疫系统的反馈机理,针对现有免疫反馈算法在系统超调后性能恶化的不足,提出了一种新型的免疫反馈算法。该算法考虑了系统超调后的免疫响应过程,补充给出了系统超调初期、中期及后期的免疫规则。仿真结果表明,基于新型免疫规则的PID控制器超调更小、响应更快,抗干扰能力强,十分适用于大惯性对象和超调量大的系统。     

扩张状态观测器在无人机纵向飞行控制中的应用

针对在设计无人机控制律时存在未建模动态和不确定扰动的特点,将未建模动态和不确定扰动视为综合扰动,引入扩张状态观测器对综合扰动项进行估计并补偿,设计出不依赖对象模型的改进PID控制器.仿真结果表明,该控制器在控制量品质、动态性能、稳态精度等方面都优于常规PID控制器.     

Variable Structure Control of Catastrophic Course in Airdropping Heavy Cargo

The mathematical model of a transport aircraft would be subjected to a sudden change when heavy cargo is dropped off in airdropping, which exerts serious influences upon the safety of the aircraft. A variable structure controller is specially designed for handling the airdrop process. The nonlinear system is linearized by input-output feedback linearization using differential geometry theories. On this basis, an inner loop system for velocity and attitude tracking control is designed by using the exponentially approaching rule of the variable structure theory. The whole flight control system is integrated with the outer loop flight altitude control. Digital simulation evidences the applicability of the system to potentially catastrophic course in airdropping heavy cargo and provides robustness against system parameter perturbation.     

基于进化策略的飞行控制系统优化

针对飞行控制系统控制器参数优化问题,提出了一种基于反馈和共享机制的改进进化策略。将各代当前最优搜索结果和共享度信息反馈到变异步长的更新公式中,达到提高算法全局搜索能力和搜索精度的目的。将此策略应用于某型飞机的横侧向飞行控制系统的参数优化之中,仿真结果表明,该优化策略能够快速有效地整定飞行控制系统参数。     

控制力矩陀螺框架高精度周期随动控制

为实现控制力矩陀螺框架伺服系统的高精度周期随动控制,采用比例积分微分(PID,Proportion Integration Differentiation)控制器结合重复控制器的控制方式,PID控制器实现框架伺服系统静态和匀速运动的高精度控制,插入式重复控制器实现对周期性输入信号的精确跟踪.对控制力矩陀螺框架系统进行了建模,设计了PID控制器与插入式重复控制器,并分析了重复控制器的稳定性条件、稳态跟踪性能和对扰动的抑制能力.仿真结果和实验结果表明:采用插入式重复控制器使控制力矩陀螺跟踪1Hz给定速度信号时的稳态跟踪误差大幅减少.PID控制器结合插入式重复控制器结构简单,两者可分开独立设计,参数设计容易.     

Acceleration sensors based modal identification and active vibration control of flexible smart cantilever plate

Some flexible appendages of spacecrafts, such as solar panels, are cantilever plate structures. Thus, vibration problem is unavoidable when there is slewing maneuver or external disturbance excitation. Vibration of such cantilever plate structures includes coupled bending and torsional motion. Furthermore, the low amplitude vibration near the equilibrium point is very difficult to be quickly suppressed due to nonlinear factors of the hardware in the system, which is harmful to stability and attitude control accuracy. To solve these problems, acceleration sensor-based modal identification and active vibration control methods are presented for the first two bending and the first two torsional modes vibration of the cantilever plate. Optimal placements of three acceleration sensors and PZT patches actuators are performed to decouple the bending and torsional vibration of such cantilever plate for sensing and actuating, and identifications are achieved by experiments. A nonlinear control method is presented to suppress both high and low amplitude vibrations of flexible smart cantilever plate significantly. Experimental comparison researches are conducted by using acceleration proportional feedback and the presented nonlinear control algorithms. The experimental results demonstrate that the presented acceleration sensor-based methods can suppress the vibration of cantilever plate effectively.