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Model predictive steering control law for double gimbal scissored-pair control moment gyros

机译:双万臂剪刀对控制力矩陀螺仪模型预测转向控制规律

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摘要

To overcome the singularity problem of control moment gyros (CMGs) and simultaneously provide a lightweight, agile, and simple dynamical system, a CMG system called a double-gimbal scissored-pair control moment gyro (DGSPCMG) was recently proposed. The DGSPCMG is a hybrid mechanism that combines scissored-pair CMGs and a double-gimbal mechanism; further, the outer singularities in this system (saturation singularities) can be escaped by steering the scissored-pair gimbals. This system generates less perturbation torque and has almost no inner singularities except at the origin and the line along the outer gimbal axis. This paper proposes model predictive control (MPC) based steering laws for the mentioned CMG system. The proposed MPC based steering laws can directly provide the optimal gimbal rate under the nonlinear constraints in real time without using the inverse of the CMG Jacobian matrix, and hence, the singularities do not have to be considered when determining the gimbal steering rate of this system. Three objective functions are considered in the steering law design: fast maneuver-weighted type, minimum control energy type, and a hybrid of these two types. The control performances of these three MPC-based steering laws are compared via numerical simulations. Results demonstrate that the hybrid type can achieve both a short rise time of the angular velocity at the initial stage of control, and smooth stabilization to the target attitude; moreover, its settling time and control effort is between those of the other two types.
机译:为了克服控制力矩陀螺陀螺壁(CMG)并同时提供轻量级,敏捷和简单的动态系统,最近提出了一种称为双轴剪刀对照时刻Gyro(DGSPCMG)的CMG系统。 DGSPCMG是一种混合机制,它结合了剪切对CMG和双金银机构;此外,该系统中的外奇异性(饱和奇迹)可以通过转向剪切对万向节来逃逸。该系统产生较少的扰动扭矩,并且除了沿着外汇轴的原点和线路外几乎没有内部奇点。本文提出了基于模型预测控制(MPC)所提到的CMG系统的转向规律。所提出的基于MPC的转向法实时可以直接在非线性约束下直接提供最佳的万能速率,而不使用CMG雅各比矩阵的逆,因此,在确定该系统的万向节转向速率时不必考虑奇点。在转向法设计中考虑了三项目标功能:快速机动加权型,最小控制能量类型和这两种类型的混合。通过数值模拟比较了这三个基于MPC的转向规律的控制性能。结果表明,混合型可以在控制的初始阶段实现角速度的短大上升时间,并使目标姿态平滑稳定;此外,其稳定时间和控制力在其他两种类型之间。

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