The control law of the flywheel in an integrated power and attitude control system (IPACS) for a spacecraft is investigated. The flywheels are used as attitude control actuators as well as energy storage device. A f...The control law of the flywheel in an integrated power and attitude control system (IPACS) for a spacecraft is investigated. The flywheels are used as attitude control actuators as well as energy storage device. A feedback control law for attitude tracking is firstly developed by using Lyapunov approach, and then a torque based control law of the flywheel is studied. The control torque vector of the flywheel is decomposed into three parts which are orthogonal to one another by using the method of singularity value decomposition (SVD). One part is used to provide the attitude control torque, another part is used to store energy with given power, and the last part is used to accomplish wheel speed equalization to avoid wheel saturation caused by large difference among the wheel spin rates. A management scheme for energy storage power using kinetic energy feedback is proposed to keep energy balance, which can avoid wheel saturation caused by superfluous energy. Numerical simulation results demonstrate the effectiveness of the control scheme.展开更多
The design problem of an integrated power and attitude control system (IPACS) for spacecrafts is investigated. A Lyapunov-typed IPACS controller is designed for a spacecraft equipped with 4 flywheels (3 orthogonal ...The design problem of an integrated power and attitude control system (IPACS) for spacecrafts is investigated. A Lyapunov-typed IPACS controller is designed for a spacecraft equipped with 4 flywheels (3 orthogonal + 1 skew). This controller keeps in the nonlinear properties of original systems, so the control result can be more precise. A control law of the flywheels is also proposed to accomplish the attitude control and energy storage simultaneously. Aiming at the limitations existing in the power conversion characteristic and the wheel's motor, a new strategy of energy management is proposed. The strategy can not only make the charged/discharged energy reaching balance in each orbital period, but also sufficiently utilize the power provided by the solar arrays. Therefore, the size and mass of solar arrays can be decreased, and the cost of spacecraft can be economized. A simulation example illustrates the validity of the designed IPACS.展开更多
通过对风电系统和飞轮储能系统运行特性的分析,针对飞轮转子设计难以安装位置传感器的特殊性问题,提出一种基于自适应非奇异快速终端滑模观测器的飞轮储能无传感器控制策略,提高转子位置角估计精度。此外,针对飞轮储能系统参考功率指令...通过对风电系统和飞轮储能系统运行特性的分析,针对飞轮转子设计难以安装位置传感器的特殊性问题,提出一种基于自适应非奇异快速终端滑模观测器的飞轮储能无传感器控制策略,提高转子位置角估计精度。此外,针对飞轮储能系统参考功率指令滞后的问题,在无传感器控制基础上,引入自适应滤波算法作为飞轮储能控制系统的功率给定,以减小功率指令滞后现象。在Typhoon HIL 602+仿真平台进行实验验证,结果表明:飞轮储能系统运行性能良好,观测器具有优越的估计性能,能满足飞轮快速充放电并有效平滑风电功率波动的控制需求,同时提高储能利用率。展开更多
A characteristic model based all-coefficient adaptive control law was recently implemented on an experimental test rig for high-speed energy storage flywheels suspended on magnetic bearings. Such a control law is an i...A characteristic model based all-coefficient adaptive control law was recently implemented on an experimental test rig for high-speed energy storage flywheels suspended on magnetic bearings. Such a control law is an intelligent control law, as its design does not rely on a pre-established mathematical model of a plant but identifies its characteristic model while the plant is being controlled. Extensive numerical simulations and experimental results indicated that this intelligent control law outperforms a μ-synthesis control law, originally designed when the experimental platform was built in terms of their ability to suppress vibration on the high-speed test rig. We further establish, through an extensive simulation, that this intelligent control law possesses considerable robustness with respect to plant uncertainties, external disturbances, and time delay.展开更多
文摘The control law of the flywheel in an integrated power and attitude control system (IPACS) for a spacecraft is investigated. The flywheels are used as attitude control actuators as well as energy storage device. A feedback control law for attitude tracking is firstly developed by using Lyapunov approach, and then a torque based control law of the flywheel is studied. The control torque vector of the flywheel is decomposed into three parts which are orthogonal to one another by using the method of singularity value decomposition (SVD). One part is used to provide the attitude control torque, another part is used to store energy with given power, and the last part is used to accomplish wheel speed equalization to avoid wheel saturation caused by large difference among the wheel spin rates. A management scheme for energy storage power using kinetic energy feedback is proposed to keep energy balance, which can avoid wheel saturation caused by superfluous energy. Numerical simulation results demonstrate the effectiveness of the control scheme.
文摘The design problem of an integrated power and attitude control system (IPACS) for spacecrafts is investigated. A Lyapunov-typed IPACS controller is designed for a spacecraft equipped with 4 flywheels (3 orthogonal + 1 skew). This controller keeps in the nonlinear properties of original systems, so the control result can be more precise. A control law of the flywheels is also proposed to accomplish the attitude control and energy storage simultaneously. Aiming at the limitations existing in the power conversion characteristic and the wheel's motor, a new strategy of energy management is proposed. The strategy can not only make the charged/discharged energy reaching balance in each orbital period, but also sufficiently utilize the power provided by the solar arrays. Therefore, the size and mass of solar arrays can be decreased, and the cost of spacecraft can be economized. A simulation example illustrates the validity of the designed IPACS.
文摘通过对风电系统和飞轮储能系统运行特性的分析,针对飞轮转子设计难以安装位置传感器的特殊性问题,提出一种基于自适应非奇异快速终端滑模观测器的飞轮储能无传感器控制策略,提高转子位置角估计精度。此外,针对飞轮储能系统参考功率指令滞后的问题,在无传感器控制基础上,引入自适应滤波算法作为飞轮储能控制系统的功率给定,以减小功率指令滞后现象。在Typhoon HIL 602+仿真平台进行实验验证,结果表明:飞轮储能系统运行性能良好,观测器具有优越的估计性能,能满足飞轮快速充放电并有效平滑风电功率波动的控制需求,同时提高储能利用率。
基金Project supported by the Fundamental Research Funds for the Central Universities,China(No.2662018QD031)
文摘A characteristic model based all-coefficient adaptive control law was recently implemented on an experimental test rig for high-speed energy storage flywheels suspended on magnetic bearings. Such a control law is an intelligent control law, as its design does not rely on a pre-established mathematical model of a plant but identifies its characteristic model while the plant is being controlled. Extensive numerical simulations and experimental results indicated that this intelligent control law outperforms a μ-synthesis control law, originally designed when the experimental platform was built in terms of their ability to suppress vibration on the high-speed test rig. We further establish, through an extensive simulation, that this intelligent control law possesses considerable robustness with respect to plant uncertainties, external disturbances, and time delay.