The simulation program of spacecraft attitude control uses the sfunction method of Simulink to establish the dynamic model and kinematic model of spacecraft attitude, and uses limod to linearize the nonlinear model.

Filename	Size	Update
MATLAB航天姿态控制仿真程序\Attitude7.m	1610	2011-03-16
MATLAB航天姿态控制仿真程序\Attitude_ode.m	856	2011-04-01
MATLAB航天姿态控制仿真程序\ode_main.m	1783	2011-04-01
MATLAB航天姿态控制仿真程序\pole.m	439	2011-04-01
MATLAB航天姿态控制仿真程序\zitai.mdl	20618	2011-04-03
MATLAB航天姿态控制仿真程序	0	2020-02-19

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