Research Article

Predictive Functional Control-Based Zenith Pass Controller Design for Roll-Pitch Seeker

Table 1

Definitions of coordinate system.

FrameDefinition

B(i) Missile body frame (regarded stationary for simplicity)
(ii) : missile nose direction
(iii) : right direction, on the yaw plane

S(i) Seeker antenna heading frame
(ii) : antenna boresight direction
(iii) : coincides with pitch gimbal axis
(iv) = seeker roll, pitch gimbal angles

P(i) Target pointing frame
(ii) : sightline direction
(iii)

DS(i) Target pointing frame
(ii) : sightline direction
(iii) : coincides with pitch gimbal angles
(iv) = desired roll, pitch gimbal angles of seeker

LOS(i) LOS frame
(ii) : sightline direction
(iii) : coincides with the z-axis of body frame
(iv) = azimuth and elevation angles of LOS based on missile body frame