An enhanced anti-disturbance attitude control law for flexible spacecrafts subject to multiple disturbances

As well-known disturbance rejection methods, active disturbance rejection control and disturbance observer-based control can effectively improve the control performances of complex systems in the presence of disturbances. However, the accurate rejection of multiple disturbances for control systems of practical engineering, for example, the attitude control system of flexible spacecraft, is still a bottleneck problem. In order to further improve the anti-disturbance capability and reduce the conservativeness, this paper proposes a novel enhanced anti-disturbance control law for the attitude control system of flexible spacecraft by combining active disturbance rejection control and disturbance observer-based control in a unified framework. More specifically, the disturbance from flexible vibration is described by an uncertain exogenous system based on the partially known information including elastic damping ratios and modal frequencies. The disturbance observer-based control is utilized to estimate and thereby reject this disturbance. On the other hand, the other disturbances such as external environmental disturbance and complex model nonlinearity are merged into a equivalent disturbance with bounded derivative, which is compensated by using the active disturbance rejection control law. Stability and robustness analysis are carried out for the disturbance observer and extended state observer. Finally, simulation results of low-earth-orbit flexible satellite are presented to verify the effectiveness of proposed methods.     

可编程控制器在水压实验机上的应用及设计

可编程控制器在恶劣环境下比继电器，接触器安全，可靠，耐用，以水压试验机编程控制器程序控制为例。阐述了液压，气动。电气联合作用下系统的可编程控制设计方法以及防干扰措施。     

感应电动机转速对定子电流暂态过程的影响

本文运用根轨迹法，分析了感应电动机转速对定子电流暂态过程的影响。并通过对稳态时定子电流在电压阶跃干扰下的暂太响应分析，验证了结论有效性。     

Adaptive control of permanent magnet synchronous machines with disturbance estimation

In this paper,an adaptive control scheme is introduced for permanent magnet synchronous machines (PMSMs)as an alternative to classical control techniques.The adaptive control strategy capitalizes on the machine’s inverse dynamics to achieve accurate tracking by using an observer to approximate disturbance in the form of friction and load torque.The controller’s output is then fed to a space vector pulse width modulation(SVPWM)algorithm to produce duty cycles for the inverter.The control scheme is validated through a set of simulations on an experimentally validated PMSM model.Results for different situations highlight its high speed tracking accuracy and high performance in compensating for friction and load disturbances of various magnitudes.     

航空发动机传感器故障鲁棒检测方法

研究发动机传感器故障准确检测问题,现代航空发动机数字电子控制系统对传感器的可靠性要求日益提高。针对航空发动机结构复杂,又工作在高温和高压下,常规采用的传感器故障检测方法的准确性易受到建模误差与外界扰动的影响,造成漏报或误报。为了提高检测精度,提出建立航空发动机数控系统传感器未知输入故障模型,采用特征结构配置的方法,通过配置闭环系统左特征向量实现故障检测残差对不确定性因素的干扰解耦,降低扰动对故障诊断结果的影响。用某型涡扇发动机数控系统传感器故障数字仿真试验表明,所设计的方法对范数有界的不确定量可以实现干扰解耦,抑制干扰对故障检测的影响,改善检测算法的鲁棒性,提高检测结果的准确性,同时满足在线运算的实时性要求。提高了航空发动机的可靠性,保证了安全飞行。     

水平阻尼作为干扰的平台式惯导统一控制方程

研究惯导系统统一控制的优化设计。传统的统一控制采用一体化设计方案,通用性不强。为简捷高效地实现惯导计算机的程序编排,提出了将水平阻尼作为干扰项的平台式惯导统一控制。通过改变系统框图结构,将无阻尼惯导系统和阻尼网络人为分离,水平阻尼网络的输出可视为干扰项。系统控制方程始终采用无阻尼条件下的表达式,惯导系统控制和阻尼网络可以实现模块化设计,使控制的实现形式和推导过程大为简化。给出了惯导计算机的运算流程,并分别在静、动基座条件下,对无阻尼、内水平阻尼和外水平阻尼状态的惯导系统做了仿真。结果表明新的统一控制模型有效体现了惯导系统的参数变化,且设计简便,具有更好的实用性。     

物联网技术在科研量化管理平台中的应用及探索

科研管理的现代化及高效化是社会发展的趋势,将物联网技术集成到科研管理平台中,能达到高效、科学、高效的效果。完善当前科研管理系统的功能,使得平台除基本的管理功能外,同时具备量化积分功能及论文共享机制等功能,为考核、评价及后续工作提供参考数据,适应当前形势下的复杂需求。     

一种关于目标罚参数的精确罚函数法

罚函数法是一种将约束优化问题转化为无约束问题的重要方法.对于一般的约束优化问题,通过加入新参数,给出了一种改进的精确罚函数和这种罚函数的精确罚定理证明,提出了求解这种罚函数的算法.实验表明该算法是有效的.     

超精密加工伺服系统滑模控制技术研究

为实现超精密加工伺服系统高精度跟踪控制，建立了交流水磁同步电机伺服系统模型，研究了带扰动观测器补偿的滑模变结构控制方法，仿真结果表明，该控制策略有效地抑制了负载扰动引起的抖振，对参数波动也有较强的适应能力，可以有效地提高系统的跟踪特性。     

知识的属性扰动规律的不等式关系

知识的属性扰动引起知识规律的变化,这些变化的规律称为扰动规律.利用单向S-粗集和单向S-粗集对偶,给出属性扰动的知识规律的上规律.下规律的概念,并对知识规律与属性扰动的知识规律进行了讨论,提出了属性扰动知识规律(上规律,下规律)的不等式定理.