Indexed by:会议论文
Date of Publication:2016-06-17
Included Journals:EI
Page Number:507-513
Abstract:A mathematical model is established for implementing hardware reconfiguration and simulation of an attitude control system for three-axis stabilized satellite. The satellite attitude quaternion, dynamics equation and kinematics equation are defined and a closed-loop system used for attitude control is designed. Computer simulation with MATLAB and FPGA instead of space borne equipment is realized, using FPGA for the host controller and some peripheral modules. The hardware simulation results are good, proving the feasibility of the scheme. Adding hardware reconfiguration into the design provides a new way for FPGA simulation of satellite attitude control system.
教授级高工
Supervisor of Master's Candidates
Main positions:控制科学与工程学院副院长
Other Post:大连理工大学电工电子国家级实验教学示范中心主任,大连理工大学电工电子国家级虚拟仿真实验教学中心主任
Gender:Male
Alma Mater:德国卡尔斯普厄科技大学
Degree:Master's Degree
School/Department:控制科学与工程学院
Discipline:Detection Technology and Automation Device
Business Address:理工北门海山楼B1607
Contact Information:QQ:1944765955
QQ联系方式 : 1944765955
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