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actuator incident angle is the sum of the actuator deflection angle and the missile angle of attack.
The Basics of Missile Guidance Control 5 The transfer function with the actuator deflection angle δ as the input and the angle of attack α as the output, shown below, can be regarded as the object being controlled for the autopilot (Fig. 1.9).
the roll moment Mx and the roll actuator deflection angle δx and the total angle of attack αT is shown
Fig. 2.5: Relationship between the roll moment Mx and the roll actuator deflection angle δx and the
coefficient, which is a function of the angle of attack and the actuator deflection angle δz for a given
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