Abstract
The paper analyzes the different model matching approaches (Exact, Pseudo-Inverse Method / PIM, Modified Pseudo-Inverse Method / MPIM) for the fault tolerant control of the short-period mode of the longitudinal model of the Boeing 747 aircraft. To overcome the drawbacks of the PIM and MPIM approaches, the paper proposes a new philosophy for the model matching problem, namely to use a set of admissible models instead of trying to best approximate a single reference one. The application shows the benefits associated with using this approach.
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