Boost Control Design for Spinning Missile.
NAVAL POSTGRADUATE SCHOOL MONTEREY CA
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A compensation scheme is presented for the pitch-yaw control system of a strategic missile which maintains stability and performance while the missile spins. The conventional missile control design for boost has uncoupled pitch, yaw and roll channels ideally suited for a non-rolling missile. The effect roll has on the conventional pitch-yaw controller is discussed and the development and simulation of a modified system is presented. Keywords Spinning missile and Thrust vector control.
- Surface-Launched Guided Missiles