With photoelectric tracking system as the research object,based on the theorem of moment of momentum and Euler dynamic equation,Nonlinear biaxial coupling dynamic model of tracking turntable is established.Effects of ...With photoelectric tracking system as the research object,based on the theorem of moment of momentum and Euler dynamic equation,Nonlinear biaxial coupling dynamic model of tracking turntable is established.Effects of moment of inertia coupling,speed coupling and the dynamic coupling between tracking turntable shafts were studied,the analytical relation between them was given in theory.Verify the change trend of theoretical model.And it provides the theory reference and model base,for the future design of the high precision tracking controller And control parameter selection and optimization.In the end,specific measures are made for structure optimization.展开更多
The tracking of orientation and angular velocity is a primary attitude control task for an on-orbit spacecraft.The problem for a rigid spacecraft tracking a desired angular velocity profile is addressed using an adapt...The tracking of orientation and angular velocity is a primary attitude control task for an on-orbit spacecraft.The problem for a rigid spacecraft tracking a desired angular velocity profile is addressed using an adaptive feedback control.An angular velocity feedback tracking algorithm is firstly developed based on the precisely known attitude dynamics of the spacecraft,and the global tracking of the control algorithm is proved based on the Lyapunov analysis.An adaptation mechanism is then designed to deal with the dynamic uncertainties of the spacecraft.Such an adaptation mechanism enables the controller to track any desired angular velocity trajectories even in the presence of uncertain inertia parameters,although it does not guarantee the inertia tensor being precisely identified.To verify the effectiveness of the proposed adaptive control policy,computer simulations on dynamic equations of a spacecraft are conducted and their results are discussed.展开更多
在不均匀光照条件下,光伏阵列输出特性呈现多峰现象,传统的最大功率点跟踪(maximum power point tracking,MPPT)方法容易陷入局部极值。为了提高复杂阴影下的跟踪速度和跟踪精度,结合改进粒子群算法(improved particle swarm optimizati...在不均匀光照条件下,光伏阵列输出特性呈现多峰现象,传统的最大功率点跟踪(maximum power point tracking,MPPT)方法容易陷入局部极值。为了提高复杂阴影下的跟踪速度和跟踪精度,结合改进粒子群算法(improved particle swarm optimization,IPSO)和自适应步长扰动观察法(adaptive perturbation and observation,AP&O)各自的特点,提出了基于IPSO-AP&O算法的改进MPPT控制方法。其中,IPSO算法采用自适应惯性权重因子,在不同搜索阶段能够充分搜索目标函数,然后与AP&O算法结合实现最大功率的稳定输出。仿真结果表明,所提出的IPSO-AP&O算法减少了传统智能算法的迭代过程,能快速跟踪到全局最大功率点,相比其余几种算法而言,在光照强度突变时均具备快速精准的双重跟踪能力,在4种场景下跟踪效率分别为99.86%、99.91%、87.63%、99.79%,能够更好地减小光伏阵列外部条件变化导致的功率损耗,所提出的MPPT控制方法能够较好地适用于光储混合系统,具备工程实用价值。展开更多
风电机组的友好型惯性响应对提高高比例风电并网系统的调频特性具有重要意义。该文首先分析最大功率点跟踪（maximum power point tracking,MPPT）运行风电机组利用转速调节实现转动惯量响应的可行性,提出利用变比例系数调节转速指令值...风电机组的友好型惯性响应对提高高比例风电并网系统的调频特性具有重要意义。该文首先分析最大功率点跟踪（maximum power point tracking,MPPT）运行风电机组利用转速调节实现转动惯量响应的可行性,提出利用变比例系数调节转速指令值的控制方案。其次针对风电机组在惯性支撑过程中对系统调频产生的不利影响,从优化惯性响应特性出发,提出风电机组基于两阶段切换的变比例系数调速策略。在此基础上,基于虚拟惯性时间常数推导惯性响应阶段的变比例系数调整策略,同时为快速恢复风电机组在惯性支撑后的MPPT运行、避免切换对系统调频的二次扰动,采用模糊控制设计该阶段变比例系数的调整策略。最后利用风电并网系统的负荷扰动仿真,论证所研究两阶段变比例系数调速策略提高系统频率响应特性的有效性,仿真结果表明该策略具有充分利用同步发电机调频能力快速恢复风电机组MPPT运行方式的特点。展开更多
文摘With photoelectric tracking system as the research object,based on the theorem of moment of momentum and Euler dynamic equation,Nonlinear biaxial coupling dynamic model of tracking turntable is established.Effects of moment of inertia coupling,speed coupling and the dynamic coupling between tracking turntable shafts were studied,the analytical relation between them was given in theory.Verify the change trend of theoretical model.And it provides the theory reference and model base,for the future design of the high precision tracking controller And control parameter selection and optimization.In the end,specific measures are made for structure optimization.
基金Supported by the Innovation Fund of Shanghai Aerospace Science and Technology(SAST 201308)
文摘The tracking of orientation and angular velocity is a primary attitude control task for an on-orbit spacecraft.The problem for a rigid spacecraft tracking a desired angular velocity profile is addressed using an adaptive feedback control.An angular velocity feedback tracking algorithm is firstly developed based on the precisely known attitude dynamics of the spacecraft,and the global tracking of the control algorithm is proved based on the Lyapunov analysis.An adaptation mechanism is then designed to deal with the dynamic uncertainties of the spacecraft.Such an adaptation mechanism enables the controller to track any desired angular velocity trajectories even in the presence of uncertain inertia parameters,although it does not guarantee the inertia tensor being precisely identified.To verify the effectiveness of the proposed adaptive control policy,computer simulations on dynamic equations of a spacecraft are conducted and their results are discussed.
文摘在不均匀光照条件下,光伏阵列输出特性呈现多峰现象,传统的最大功率点跟踪(maximum power point tracking,MPPT)方法容易陷入局部极值。为了提高复杂阴影下的跟踪速度和跟踪精度,结合改进粒子群算法(improved particle swarm optimization,IPSO)和自适应步长扰动观察法(adaptive perturbation and observation,AP&O)各自的特点,提出了基于IPSO-AP&O算法的改进MPPT控制方法。其中,IPSO算法采用自适应惯性权重因子,在不同搜索阶段能够充分搜索目标函数,然后与AP&O算法结合实现最大功率的稳定输出。仿真结果表明,所提出的IPSO-AP&O算法减少了传统智能算法的迭代过程,能快速跟踪到全局最大功率点,相比其余几种算法而言,在光照强度突变时均具备快速精准的双重跟踪能力,在4种场景下跟踪效率分别为99.86%、99.91%、87.63%、99.79%,能够更好地减小光伏阵列外部条件变化导致的功率损耗,所提出的MPPT控制方法能够较好地适用于光储混合系统,具备工程实用价值。
文摘风电机组的友好型惯性响应对提高高比例风电并网系统的调频特性具有重要意义。该文首先分析最大功率点跟踪（maximum power point tracking,MPPT）运行风电机组利用转速调节实现转动惯量响应的可行性,提出利用变比例系数调节转速指令值的控制方案。其次针对风电机组在惯性支撑过程中对系统调频产生的不利影响,从优化惯性响应特性出发,提出风电机组基于两阶段切换的变比例系数调速策略。在此基础上,基于虚拟惯性时间常数推导惯性响应阶段的变比例系数调整策略,同时为快速恢复风电机组在惯性支撑后的MPPT运行、避免切换对系统调频的二次扰动,采用模糊控制设计该阶段变比例系数的调整策略。最后利用风电并网系统的负荷扰动仿真,论证所研究两阶段变比例系数调速策略提高系统频率响应特性的有效性,仿真结果表明该策略具有充分利用同步发电机调频能力快速恢复风电机组MPPT运行方式的特点。
文摘多微源独立微网中,传统下垂控制的输出频率动态响应速度快,虚拟同步发电机(virtual synchronous generator,VSG)控制可改善频率响应特性,但无法兼顾功率和频率的动态调节性能。针对此问题,提出一种改进的转动惯量自适应控制(improved adaptive control of inertia,IACI)。首先,在同步旋转坐标系下建立VSG数学模型,并分析转动惯量对VSG输出特性的影响;其次,在VSG控制的基础上通过在转动惯量控制中引入频率变化量形成VSG转动惯量自适应控制,并给出频率跟踪系数、转动惯量和阻尼系数等参量的整定方法;最后利用Matlab/Simulink对比VSG控制和IACI控制在VSG并入微网和负载扰动条件下的有功和频率响应曲线,在由两台1k W的VSG组成的独立微网实验平台上进行实验验证,结果表明所提控制策略可避免VSG并入微网过程中的有功振荡,且可以有效优化频率响应曲线。
