In today's aircraft,the hardware redundancy is driven by the critical surfaces resulting in single point-failures.Reconfiguration technology remoVes the single surface criticality by employing control surfaces wit...In today's aircraft,the hardware redundancy is driven by the critical surfaces resulting in single point-failures.Reconfiguration technology remoVes the single surface criticality by employing control surfaces with aerodynamic redundancy.This paper studies a control reconfiguration scheme based on Control Mixer Concept.A technique for the design of a control mixer for an aircraft with damaged surfaces/actuators using the pseudo-inverse is developed and applied.This paper discusses its applications and limitations based on linear analysis and computer simulation.展开更多
恒温混匀仪是医学和生物学等领域中常用的仪器,精确的温度控制是确保恒温混匀仪正常工作的关键。本文提出了一种基于TEC(Thermal Electronic Cooler)的智能PID(Proportional Integral Derivative)温度控制系统制,通过离散测量数据库中...恒温混匀仪是医学和生物学等领域中常用的仪器,精确的温度控制是确保恒温混匀仪正常工作的关键。本文提出了一种基于TEC(Thermal Electronic Cooler)的智能PID(Proportional Integral Derivative)温度控制系统制,通过离散测量数据库中的多项式回归,对PID常数进行表征,为目标温度选择正确的值。结果表明:该系统的超调小于0.005℃,准确度小于±0.05℃,可确保在不同的环境温度下保持最佳的工作性能,实现最优的温控。展开更多
文摘In today's aircraft,the hardware redundancy is driven by the critical surfaces resulting in single point-failures.Reconfiguration technology remoVes the single surface criticality by employing control surfaces with aerodynamic redundancy.This paper studies a control reconfiguration scheme based on Control Mixer Concept.A technique for the design of a control mixer for an aircraft with damaged surfaces/actuators using the pseudo-inverse is developed and applied.This paper discusses its applications and limitations based on linear analysis and computer simulation.
文摘恒温混匀仪是医学和生物学等领域中常用的仪器,精确的温度控制是确保恒温混匀仪正常工作的关键。本文提出了一种基于TEC(Thermal Electronic Cooler)的智能PID(Proportional Integral Derivative)温度控制系统制,通过离散测量数据库中的多项式回归,对PID常数进行表征,为目标温度选择正确的值。结果表明:该系统的超调小于0.005℃,准确度小于±0.05℃,可确保在不同的环境温度下保持最佳的工作性能,实现最优的温控。
