Title:
Missile-Attitude-control
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Description: One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude
2, the use of linmod linearization of the nonlinear model
Attitude model linearization, the use of pole configuration (pole) is used to obtain the control parameters
4, the control parameters into the nonlinear model simulation control effect.
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File list (Check if you may need any files):
ode45_linmod\ode_main.m
............\Attitude_ode.m
............\pole.m
............\Attitude7.m
............\zitai.mdl
ode45_linmod
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