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Research on the Robustness of PISS Integral Sliding Mode Control of Supersonic Missiles

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Figure

Figure 1 shows the overload of the system, the rise time is 5s and there exists chattering phenomenone
Figure 3. The curve of attack angle.
Figure 13 to figure 16 show the control effect of PISS control law.
Figure 23.  The curve of attack angle

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