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论文类型：会议论文
发表时间：2016-06-17
收录刊物：EI
页面范围：507-513
摘要：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.