典型文献
Attitude Control of Spherical Liquid-Filled Spacecraft Based on High-Order Fully Actuated System Approaches
文献摘要：
The attitude of spherical liquid-filled spacecraft is controlled based on the high-order fully actuated system approaches.The rigid-fluid coupling dynamic equation can be established in terms of the Euler angles of the spacecraft and the angular velocities of the liquid fuel.According to the dynamic equation,three kinds of input selections are presented.In the case of one control input,the dynamic equation is transformed into the third-order or the second-order differential equations of the Euler angle by the high-order fully actuated system approaches.Then a control law is designed to track the target.The effectiveness of the control law is demonstrated by numerical simulations.
文献关键词：
中图分类号：
作者姓名：
XIAO Fuzheng;CHEN Liqun
作者机构：
School of Science,Harbin Institute of Technology(Shenzhen),Shenzhen 518055,China
文献出处：
引用格式：
[1]XIAO Fuzheng;CHEN Liqun-.Attitude Control of Spherical Liquid-Filled Spacecraft Based on High-Order Fully Actuated System Approaches)[J].系统科学与复杂性学报（英文版）,2022(02):471-480
A类：
B类：
Attitude,Control,Spherical,Liquid,Filled,Spacecraft,Based,High,Order,Fully,Actuated,System,Approaches,attitude,spherical,liquid,filled,spacecraft,controlled,high,order,fully,actuated,system,approaches,rigid,fluid,coupling,dynamic,can,be,established,terms,Euler,angles,angular,velocities,fuel,According,three,kinds,input,selections,are,presented,In,case,one,transformed,into,third,second,differential,equations,by,Then,law,designed,track,target,effectiveness,demonstrated,numerical,simulations
AB值：
0.628254
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