International Journal of Aerospace Engineering / 2021 / Article / Fig 11

Research Article

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

Figure 11

Response of gimbal rate without controller for a missile rotation of 10 deg/s—elevation axis (a); azimuth axis (b).
(a)
(b)