同时含状态和输入时滞系统的最优滑模控制

研究了一类线性时滞系统的变结构控制器的设计问题。为了简化变结构控制器的设计,首先通过非奇异线性变换将含状态时滞和输入时滞的线性系统化为无时滞系统。其次,在新坐标下,设计变结构控制器。结合二次型性能指标最优控制方法,给出了线性无时滞系统最优滑模的综合设计方法。引入趋近律方法设计控制律,有效的削弱了抖振并能保证系统在有限的时间内到达滑模面。最后,提出并证明了原系统渐近稳定的充分条件。仿真例证了该方法的有效性。     

DMD微镜非线性特性数值模拟

DMD微镜系统的动态特性分析是非常复杂的，这是因为在系统中存在静电和机械两个非线性耦合的物理场。文中首先分析了无阻尼微镜系统的固有频率；然后采用直接积分法详细分析了系统的相轨迹曲线以及系统的正弦激励响应，通过数值模拟发现系统的相轨迹存在一个稳定点和一个非稳定平衡点；在正弦激励下，系统的共振频率随施加电压增大而减小、振动平衡位置随电压增大发生偏移等现象。     

State transfer control of quantum systems on the Bloch sphere

The state transfer under control fields is analyzed based on the Bloch sphere representation of a single qubit. In order to achieve the target from an arbitrary initial state to a target state, the conditions that parameters should satisfy are deduced separately in two different requirements: One is in the case of the rotation angle around the x-axis being fixed and another is in the situation with a given evolution time. Several typical states trajectories are demonstrated by numerical simulations on the Bloch sphere. The relations between parameters and the trajectories are analyzed.     

航天器三维空间追逃问题研究

针对固定时间下的两航天器三维空间追逃问题,采用协同进化算法将复杂的双边最优规划问题简化成对追逃过程中纳什均衡点的搜索,进而得出追逃双方的最优对抗策略及解算方法。考虑在保证算法计算精度的前提下缩短计算时间,将对策模型进行简化处理,以航天器推力指向角为控制量对协同进化算法进行编码设计,利用B样条基函数对编码进行逼近拟合。两航天器均为连续小推力作用,以二者的末端相对距离作为支付函数,逃逸器希望支付最大,追踪器希望支付最小,并依此建立共享适应度函数。所提方法中对协同算子进行改进设计,提高算法空间搜索能力,并采用精英保留策略提高算法的收敛速度。仿真算例得到追逃双方的最优控制策略及相应的追逃轨迹,表明所提方法的能够解决此类航天器追逃问题。     

递阶稳态优化下非线性大工业过程的迭代学习控制

对递阶稳态优化下非线性大工业过程施行迭代学习控制 ,目的是进一步改善大工业过程的动态品质 .建立迭代学习控制的基本结构 ,提出迭代学习控制算法关于控制系统的ε-收敛性和期望目标轨线的δ -可达性的概念 ,对具有死区与滞后的饱和非线性大工业过程控制系统给出加权超前开环PD-型迭代学习算法 .利用 Bellman-Gronwall不等式和λ范数理论 ,论证了算法的收敛性 .数字仿真表明 ,迭代学习控制能有效改善递阶稳态下非线性大工业控制系统的动态品质 .     

一类不确定时滞系统的滑模控制

考虑了一类同时存在状态不确定性和控制不确定性的时滞系统的滑模控制问题,通过采用李亚普诺夫方法和线性矩阵不等式(LMI)技术,给出了闭环系统渐近稳定的充分条件,而且滑模控制律和滑模面的设计可以利用线性矩阵不等式的解得到,证明了该滑模控制律能保证状态轨迹被驱动到指定的切换面上。仿真实验表明了算法的有效性。     

PD-type iterative learning control for nonlinear time-delay system with external disturbance

1 .INTRODUCTIONTheiterativelearning control method was proposedby Ariomoto et al[1]for the control system, whichcan performthe same task repetitively . The basiclearning controller for generating the present con-trol input is based on the previous control historyand a learning mechanism.In the last two decadesiterative learning control has been extensivelystudied and achieved significant progress in boththeory and application,and becomes the one of themost active fields inintelligent cont…     

Deterministic approaches for noncoherent communicationswith chaotic carriers

1.INTRODUCTION Since1990s,chaoticsignalshavebecomepromising carriersincommunications[1].Severalschemeshave beendevelopedsuchaschaoticmasking[2],chaotic modulation[3],chaosspreadingspectrumcommunica tion[4],chaosshiftkeying(CSK)[5].Theadvantages ofutilizingchaoticdynamicsinsuchschemesinclude thebroadband,apparentlystochastic,δ likeautocor relation,natureofthesignalandtheeasewithwhich chaoticdatamaybegenerated.Andtheseschemes exploiteitherthesynchronizationprinciplesforchaot icsignals(…     

弹道导弹目标群轨迹建模与仿真

针对弹道导弹在空间中形成的目标群轨迹具有复杂性和多阶段的特点,提出一种弹道导弹目标群轨迹分阶段建模方法。由于不同阶段下目标群运动特性存在差异,基于分阶段建模的思想,在定义相应坐标系的基础上,建立了对称释放结构下的中段诱饵释放模型;在考虑数量质量、初始状态及消亡条件等因素下,设计了助推段多批次碎片轨迹产生过程。实验仿真了地固系下弹道导弹主体弹道、诱饵释放过程以及多批次碎片轨迹。结果表明,该方法在选择恰当参数的条件下可近似逼近真实情况。     

A Maturing of Systems Thinking? Evidence from Three Perspectives

This paper reviews trends in systems theory/thinking from the 1970s to the early 2000s. It proposes a maturation of the field based on certain conceptual and methodological advances that have sought to liberate systems thinking from earlier strictures. An edited dialogue among three prominent systems thinkers from different systems schools—Merrelyn Emery, Bob Flood, and Eric Wolstenholme—provides evidence. Similarities and differences are identified, complementarities among the schools are derived and analyzed, and trajectories for future research are indicated.     

Discrete sliding mode prediction control of uncertain switched systems

The robust stabilization problem for a class of uncertain discrete-time switched systems is presented. A predictive sliding mode control strategy is proposed, and a discrete-time reaching law is improved. By applying a predictive sliding surface and a reference trajectory, combining with the state feedback correction and rolling optimization method in the predictive control strategy, a predictive sliding mode controller is synthesized, which guarantees the asymptotic stability for the closed-loop systems. The designed control strategy has stronger robustness and chattering reduction property to conquer with the system uncertainties. In addition, a unique nonswitched sliding surface is designed. The reason is to avoid the repetitive jump of the trajectories of the state components of the closed-loop system between sliding surfaces because it might cause the possible instability. Finally, a numerical example is given to illustrate the effectiveness of the proposed theory.     

Constrained predictive control of nonlinear stochastic systems

The receding horizon control (RHC) problem is considered for nonlinear Markov jump systems which can be represented by Takagi-Sugeno fuzzy models subject to constraints both on control inputs and on observe outputs. In the given receding horizon, for each mode sequence of the T-S modeled nonlinear system with Markov jump parameter, the cost function is optimized by constraints on state trajectories, so that the optimization control input sequences are obtained in order to make the state into a terminal invariant set. Out of the receding horizon, the stability is guaranteed by searching a state feedback control law. Based on such stability analysis, a linear matrix inequality approach for designing receding horizon predictive controller for nonlinear systems subject to constraints both on the inputs and on the outputs is developed. The simulation shows the validity of this method.         

载人火星任务混合推进轨道方案

以未来载人火星探测任务为背景,提出了混合推进的轨道方案,即行星中心轨道段采用脉冲推力变轨,行星际航行轨道段采用小推力变轨的策略。建立了日心段三自由度动力学模型,利用“能量等高线”图选取了几组典型脉冲往返轨道作为标称轨道：最小能量税遁,快速转移税逆和短期停留轨道。在此基础上设计了与之对应的行星际航行段小推力最优转移轨道,得到混合推进的轨道方案。最后通过与脉冲轨道的燃料消耗对比,分析了混合推进轨道方案的可行性。研究表明,此类方案较好地结合了脉冲变轨飞行时间短的优势和小推力变轨省燃料．任务灵活的优势.     

终端和过载约束下的双圆弧制导律

为满足导弹打击目标的落角、时间与过载约束,设计了一种双圆弧轨迹和相应制导律。在初始速度方向角和终端落角的约束下,利用双圆弧的相切关系推导了双圆弧轨迹的解析形式及其可行解集。根据双圆弧轨迹结果由切点决定的特征,推导得出使轨迹满足过载约束、终端约束或能量最优的切点选择方法。之后利用圆弧几何特性和弹目相对运动关系,设计了不依赖弹目距离信息的双圆弧制导律。数值仿真结果表明,双圆弧制导律能够满足复杂约束,且与最优制导律相比,可获得能量最优性相当的结果。     

基于hp自适应伪谱法的N脉冲轨道优化设计

在实效性要求高的空间操控任务中,脉冲轨道的优化设计必不可少。针对脉冲轨道转移和交会的优化设计问题,基于hp自适应伪谱法设计一种通用方法,以直接法计算为主,综合使用间接法主矢量理论交互式规划出最优N脉冲轨道的机动方案。该方法以hp自适应伪谱法直接求解首末端双脉冲机动,依据间接法最优脉冲机动满足的主矢量必要条件进行检验,通过增加脉冲或者首末端漂移进行交互式规划,逐步确定出最优脉冲数目N的值,再采用hp自适应伪谱法求解出各脉冲速度增量的矢量与施加时刻,获得脉冲轨道的优化设计。提供2个仿真场景算例,求解过程和结果表明,该方法对初值敏感度小、鲁棒性强、收敛快、实用有效,可以便捷处理脉冲轨道的优化设计问题。     

多级影响图在空战机动决策中的应用

利用多级影响图来模拟飞行员在不确定情况下近距格斗时的连续机动决策,并把动力学质点模型和飞行员的偏好考虑到模型中.针对求解多级影响图计算量大的问题,本文把它转化为分层最优化问题,利用进化算法求得最优机动决策.最后的仿真结果表明该模型的有效性.     

CONVERGENCE OF A CLASS OF MULTI-AGENT SYSTEMS IN PROBABILISTIC FRAMEWORK

Multi-agent systems arise from diverse fields in natural and artificial systems, and a basic problem is to understand how locally interacting agents lead to collective behaviors （e.g., synchronization） of the overall system. In this paper, we will consider a basic class of multi-agent systems that are described by a simplification of the well-known Vicsek model. This model looks simple, but the rigorous theoretical analysis is quite complicated, because there are strong nonlinear interactions among the agents in the model. In fact, most of the existing results on synchronization need to impose a certain connectivity condition on the global behaviors of the agents＇ trajectories （or on the closed-loop dynamic neighborhood graphs）, which are quite hard to verify in general. In this paper, by introducing a probabilistic framework to this problem, we will provide a complete and rigorous proof for the fact that the overall multi-agent system will synchronize with large probability as long as the number of agents is large enough. The proof is based on a detailed analysis of both the dynamical properties of the nonlinear system evolution and the asymptotic properties of the spectrum of random geometric graphs.     

无推力可控弹可达域和投放域计算

传统炸弹的火控系统中主要采用连续计算命中点CCIP和连续计算投放点CCRP攻击方式。对无推力可控弹在一定投放条件下构成的弹着点区域进行了计算分析，采用对角度积分的快速积分算法，快速确定区域边界。根据无推力可控弹所具有的可达域的概念，提出了连续计算可达域CCAR和连续计算投放域CCRR攻击方式。充分利用了可控弹的可操纵性，降低了瞄准误差要求。     

月地应急返回轨道优化设计

针对载人登月任务中的应急返回问题,对基于三脉冲变轨的方案进行优化设计。以圆型限制性三体问题(circular restricted three body problem, CR3BP)模型为基础,采用球坐标形式的月球返回运动模型。考虑环月轨道面、月球最小安全距离、终端近地距等约束,采用MultiStart算法对月地应急返回轨道进行全局优化。通过大量的计算仿真,验证了所提算法的有效性和可行性,并分析了不同轨道参数对性能指标的影响。研究结论对未来载人登月应急返回方案的设计具有重要的参考价值。     

捕获轨迹机构连续同步控制试验方式研究

捕获轨迹试验装置（captive trajectory simulation system, CTS）是在风洞中进行外挂物分离试验、对分离轨迹进行模拟的多自由度机构。首先对风洞中CTS的连续动态轨迹试验方式的基本过程和实现进行了说明。主要对多自由度机构在动态生成轨迹中的连续同步控制和天平信号的实时处理问题进行了详细介绍。采用了非线性实时迭代优化算法设计实现CTS多自由度机构的缓冲同步控制算法,解决动态轨迹的连续同步控制问题;运用零相位偏移的数字滤波器设计小滞后的实时滤波算法,实时提取天平信号的有效信号。最后将CTS连续动态轨迹试验方式的风洞试验数据与传统的位置控制方式的试验数据进行了对比。结果表明,在相同条件下,连续动态轨迹试验方式减少风洞CTS的试验时间约60%,所产生的分离轨迹数据与位置控制方式一致。