In remote sensing or laser communication space missions, spacecraft need fast maneuver and fast stabilization in order to accomplish agile imaging and attitude tracking tasks. However, fast attitude maneuvers can easi...In remote sensing or laser communication space missions, spacecraft need fast maneuver and fast stabilization in order to accomplish agile imaging and attitude tracking tasks. However, fast attitude maneuvers can easily cause elastic deformations and vibrations in flexible appendages of the spacecraft. This paper focuses on this problem and deals with the combined control of fast attitude maneuver and sta- bilization for large complex spacecraft. The mathematical model of complex spacecraft with flexible appendages and momentum bias actuators on board is presented. Based on the plant model and combined with the feedback controller, modal parameters of the closed-loop system are calculated, and a multiple mode input shaper utilizing the modal information is designed to suppress vibrations. Aiming at reducing vibrations excited by attitude maneuver, a quintic polynomial form rotation path planning is proposed with constraints on the actuators and the angular velocity taken into account. Attitude maneuver simulation results of the control systems with input shaper or path planning in loop are sepa- rately analyzed, and based on the analysis, a combined control strategy is presented with both path planning and input shaper in loop. Simulation results show that the combined control strategy satisfies the complex spacecraft＇s require- ment of fast maneuver and stabilization with the actuators＇ torque limitation satisfied at the same time.展开更多
为了解决船上吊车的防摆问题,实现负载快速准确的定位,建立了系统的空间三维数学模型,提出了基于输入整形的前馈开环消摆控制策略。对定摆长条件下系统控制输入设计了ZVD(Zero Vibration and Derivative)输入整形器;基于输入整形器灵敏...为了解决船上吊车的防摆问题,实现负载快速准确的定位,建立了系统的空间三维数学模型,提出了基于输入整形的前馈开环消摆控制策略。对定摆长条件下系统控制输入设计了ZVD(Zero Vibration and Derivative)输入整形器;基于输入整形器灵敏度曲线,利用矢量求和的方法设计了对称3峰的EI(Extra Insensitive)输入整形器,解决了在绳长变化时吊车系统防摆的控制问题;指出了输入整形对海浪影响的抑制作用。仿真结果验证了输入整形对于船上吊车防摆控制的有效性。展开更多
基金supported by the Excellent Young Scholars Research Fund of Beijing Institute of Technology(2012YG0101)the National Natural Science Foundation of China(11302026)
文摘In remote sensing or laser communication space missions, spacecraft need fast maneuver and fast stabilization in order to accomplish agile imaging and attitude tracking tasks. However, fast attitude maneuvers can easily cause elastic deformations and vibrations in flexible appendages of the spacecraft. This paper focuses on this problem and deals with the combined control of fast attitude maneuver and sta- bilization for large complex spacecraft. The mathematical model of complex spacecraft with flexible appendages and momentum bias actuators on board is presented. Based on the plant model and combined with the feedback controller, modal parameters of the closed-loop system are calculated, and a multiple mode input shaper utilizing the modal information is designed to suppress vibrations. Aiming at reducing vibrations excited by attitude maneuver, a quintic polynomial form rotation path planning is proposed with constraints on the actuators and the angular velocity taken into account. Attitude maneuver simulation results of the control systems with input shaper or path planning in loop are sepa- rately analyzed, and based on the analysis, a combined control strategy is presented with both path planning and input shaper in loop. Simulation results show that the combined control strategy satisfies the complex spacecraft＇s require- ment of fast maneuver and stabilization with the actuators＇ torque limitation satisfied at the same time.
文摘为了解决船上吊车的防摆问题,实现负载快速准确的定位,建立了系统的空间三维数学模型,提出了基于输入整形的前馈开环消摆控制策略。对定摆长条件下系统控制输入设计了ZVD(Zero Vibration and Derivative)输入整形器;基于输入整形器灵敏度曲线,利用矢量求和的方法设计了对称3峰的EI(Extra Insensitive)输入整形器,解决了在绳长变化时吊车系统防摆的控制问题;指出了输入整形对海浪影响的抑制作用。仿真结果验证了输入整形对于船上吊车防摆控制的有效性。
