成像卫星鲁棒性调度策略研究

针对不确定条件下的成像卫星调度问题,分析了鲁棒性调度要求,提出了鲁棒性调度策略,将成像卫星调度分为鲁棒性调度方案生成和鲁棒性调度方案动态调整两个阶段。在鲁棒性调度方案生成阶段,以调度方案收益和鲁棒性为优化目标,建立了成像卫星鲁棒性调度模型。在鲁棒性调度方案动态调整阶段,以调度方案收益和新老调度方案差异为优化目标,建立了成像卫星动态调度模型。仿真实例验证了成像卫星鲁棒性调度策略和模型的有效性。     

大型不确定前馈型系统的分散鲁棒镇定

研究了大型不确定前馈型系统的鲁棒分散镇定问题。因为系统具有前馈型结构,采用自下而上的迭代分析方法,同时注意运用互联非线性系统有界性和稳定性判据。将设计任务转化为镇定底层子系统和其他子系统的标称部分,并可以明确构造简单的饱和控制律。该方法利用系统的结构特性,不太依赖李雅普诺夫函数,也不需要通常的LMI技巧。仿真说明该方法的有效性。     

基于凸多面体不确定网络化系统的鲁棒无源滤波

研究一类同时具有时变时延和测量数据丢失的不确定网络化系统的鲁棒无源滤波器设计问题。时变时延假设在一个已知的界内随机变化。测量数据的丢失是随机发生的,假设满足Bernoulli分布随机序列。采用线性矩阵不等式方法,给出了全阶和降阶的鲁棒无源滤波器存在的充分条件。所设计的滤波器使得滤波误差系统是均方指数稳定并满足给定的无源指标。最后数值仿真表明所提方法的有效性。     

船舶航向与柴油主机联合LPV鲁棒控制及仿真

船舶航向与柴油机推进装置是紧密耦合的,但长期以来对它们的控制是完全独立的.根据线性变参数(LPV)系统设计原理,提出了基于LPV的船舶航向与主机联合控制.建立了以船速等为变参数的船舶航向与主机联合控制的LPV模型,采用LPV多胞设计方法,通过状态反馈对闭环极点进行配置,分别设计具有H∞鲁棒性能的航向与主机LPV控制器,实现二者的联合控制.以5446箱班轮为被控制对象,仿真验证了航向与主机LPV控制器在风浪干扰下联合控制的有效性.     

两类不确定奇异时滞系统鲁棒稳定的相关型判据

研究了不确定奇异时滞系统的鲁棒稳定性问题。首先以线性矩阵不等式的形式给出了奇异时滞系统正则,无脉冲模且零解渐近稳定的一种新的时滞相关型判据。通过引入新的参数避免了利用不等式处理交叉项,从而使该判据具有较小的保守性。最后,利用研究结果,给出了两类不确定奇异时滞系统新的时滞相关型鲁棒稳定性判据。     

具有对偶极点的不稳定过程的鲁棒控制

为了进一步完善不稳定系统的鲁棒控制器设计方法,将具有对偶极点的不稳定过程分成纯不稳定过程与一般的稳定过程两部分,对于纯不稳定过程采用先成形再镜像映射的方法,而对于一般的稳定过程则基于极点对消原则直接设计控制器,最后用闭环增益成形算法求解鲁棒控制器。将所设计的鲁棒控制器应用于磁浮列车的悬浮控制中,从仿真结果可以看出,控制效果可以达到小超调(<8%)、无静差、调节时间快(<0.1 s)、对模型摄动具有鲁棒稳定性。     

Adaptive SPC monitoring scheme for DOE-based APC

Automatic process control （APC） based on design of experiment （DOE） is a cost-efficient approach for variation reduction. The process changes both in mean and variance owing to online parameter adjustment make it hard to apply traditional SPC charts in such DOE-based APC applied process. An adaptive SPC scheme is developed, which can better track the process transitions and achieve the possible SPC run cost reduction when the process is stable. The control law of SPC parameters is designed by fully utilizing the estimation properties of the process model instead of traditionally using the data collected from the production line. An example is provided to illustrate the proposed adaptive SPC design approach.     

Robust H∞ control for neutral stochastic uncertain systems with time-varying delay

The problem of robust H∞ control for uncertain neutral stochastic systems with time-varying delay is discussed. The parameter uncertaintie is assumed to be time varying norm-bounded. First, the stochastic robust stabilization of the stochastic system without disturbance input is investigated by nonlinear matrix inequality method. Then, a full-order stochastic dynamic output feedback controller is designed by solving a bilinear matrix inequality (BMI), which ensures a prescribed stochastic robust H∞ performance level for the resulting closed loop system with nonzero disturbance input and for all admissible uncertainties. An illustrative example is provided to show the feasibility of the controller and the potential of the proposed technique.     

Missile robust gain scheduling autopilot design using full block multipliers

Reduction of conservatism is one of the key and difficult problems in missile robust gain scheduling autopilot design based on multipliers. This article presents a scheme of adopting linear parameter-varying (LPV) control approach with full block multipliers to design a missile robust gain scheduling autopilot in order to eliminate conservatism. A model matching design structure with a high demand on matching precision is constructed based on the missile linear fractional transformation (LFT) model. By applying full block S-procedure and elimination lemma, a convex feasibility problem with an infinite number of constraints is formulated to satisfy robust quadratic performance specifications. Then a grid method is adopted to transform the infinite-dimensional convex feasibility problem into a solvable finite-dimensional convex feasibility problem, based on which a gain scheduling controller with linear fractional dependence on the flight Mach number and altitude is derived. Static and dynamic simulation results show the effectiveness and feasibility of the proposed scheme.     

基于仿真模型的鲁棒协同优化方法研究

复杂产品往往由多个子系统通过复杂的耦合方式组成.针对复杂产品的多学科鲁棒设计优化技术已得到广泛应用.为了使用仿真模型进行多学科鲁棒设计优化,提出了SUA-RCO和DRS-RCO两种方法.在SUA-RCO方法中,仿真模型首先被拟合为近似的数学模型,然后利用近似数学模型进行RCO计算.系统的不确定性由SUA方法进行计算.为了解决大参数方差问题,DRS-RCO方法将仿真模型近似拟合为双响应面形式,分别使用两个响应面来拟合均值和方差.然后,进行协同优化计算.