A Novel Self-Tuning Fuzzy Logic-Based PID Controllers for Two-Axis Gimbal Stabilization in a Missile Seeker

<div class="floats-full-page floats-full-page-figure"><h2>Figure 12</h2><div class="floats-full-page-caption"><div>Step response of elevation gimbal with conventional and fuzzy PID controllers for a missile rotation of 10 deg/s.</div></div><div class="floats-full-page-content"><table class="figure-group"><tr class="fig-image"><td><object data="https://static-01.hindawi.com/articles/ijae/volume-2021/8897556/figures/8897556.fig.0012.svgz" name="8897556.fig.0012" type="image/svg+xml"></object></td></tr></table></div></div>

Figure 12 | A Novel Self-Tuning Fuzzy Logic-Based PID Controllers for Two-Axis Gimbal Stabilization in a Missile Seeker

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Figure 12: A Novel Self-Tuning Fuzzy Logic-Based PID Controllers for Two-Axis Gimbal Stabilization in a Missile Seeker

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Figure 12

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<p><em>International Journal of Aerospace Engineering </em>serves the international aerospace engineering community through the dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles.</p>


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<p>Chief Editor, Professor Zhao, is based at the University of Canterbury and his research interests include applying theoretical, numerical and experimental approaches to study combustion instability, thermoacoustics and aerodynamics.</p>


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