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LMIs in Control/pages/LMI for Attitude Control of BBT Missiles
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LMI for Attitude Control of BTT Missles, Roll Channel
For this dynamic model of a Bank-to-Turn (BTT) missile, we will consider a simplified attitude system model for the roll channel in the system. We aim to achieve a non-rotating motion of missiles. It is worthwhile to note that the attitude control design for the pitch channel and the yaw/roll channel can be solved exactly in the same way while representing matrices of the system are different.