Project VirtUE
Dynamic System Identification
ST: SYSTEM THEORY
ST1 Polynomial input-output models
ST2 Equivalence relations for MFD models
ST3 State space canonical forms
ST4 Links between state space and input-output models
ST5 Realization of MISO input-output sequences
ST6 Realization of MIMO input-output sequences
One of the most celebrated applications of System Theory concerns the use of Kalman filtering in the guide system of Apollo spacecrafts. The accuracy in trajectory estimation offered by this algorithm allowed, in fact, early corrections leading to successful Apollo 11 mission using Saturn V vector (image is courtesy of NASA).
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