NLGA based Active Control in Aerospace: fault tolerability, disturbance rejection, and parameter estimation
A new control scheme has been presented in this thesis. Based on the NonLinear Geometric Approach, the proposed Active Control System represents a new way to see the reconfigurable controllers for aerospace applications. The presence of the Diagnosis module (providing the estimation of generic si...
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| Format: | Doctoral Thesis |
| Language: | en |
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Alma Mater Studiorum - Università di Bologna
2015
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| Online Access: | http://amsdottorato.unibo.it/7113/ |