LMIs in Control/pages/LMI for Attitude Control of BTT Missiles: Revision history

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21 November 2021

  • curprev 22:5022:50, 21 November 2021 imported>Scarris8 4,463 bytes +4,463 Created page with "<big><big>'''LMI for Attitude Control of BTT Missles, Roll Channel'''</big></big> The dynamic model of a bank-to-burn (BTT) missile can be simplified for practical application. The dynamic model for a BTT missile is given by the same model used for nonrotating missiles. However, in this case we can assume that the missile is axis-symmetrically design, and thus Jx = Jy. We assume that the roll channel is independent of the pitch and yaw channels. == '''The System''' ==..."
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