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Dynamics of a controlled anti-aircraft missile...

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t [s]    t [s]

Fig. 13. Time-dependent angular accelerations of the launcher without (a) and with (b) correction, i)_pv and ^pv, respectively

Fig. 14. Time-dependent angular displacements of the launcher turret during pre-programmed control without (a) and with (b) correction, d_v and p_v, respectively

* W

i	E)
	tł :

■lool--

0 0.2 0.4 0.6 0.8 1.0 1.2 1.4

t [s]

Fig. 15. Time-dependent angular velocities of the launcher turret during pre-programmed control without (a) and with (b) correction, d_v and p_v, respectively