Integrated Guidance and Control Design of Rolling-Guided Projectile Based on Adaptive Fuzzy Control with Multiple Constraints

Figure 4

Experimental curves of operating condition 2. (a) Trajectory of projectile and target. (b) Lateral overload. (c) Quasi sideslip angle. (d) Equal yaw canard angle. (e) Yaw canard angle. (f) LOS azimuth angle rate. (g) Yaw angle. (h) and disturbance . (i) and disturbance .

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(i)