Modern Homing Missile Guidance Theory and Techniques

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Here, we start by considering a general nonlinear dynamics model of the system to be controlled (i.e., the “plant”). This dynamics model can be expressed as x f$ ( )t t= ( (x u), ( )t t, ) . (1) In Eq. 1, x is the n-dimensional state vector of real elements ( )x u! !R Rn m, is the control vector, and

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