In this report a design method for linear proportional and linear dynamic output feedback regulators for discrete time systems is presented. It is shown how this design method may be applied to the design of aircraft automatic control systems.
Output feedback regulators for aircraft automatic control systems
Regler mit Rueckkopplung des Ausgangssignals fuer automatische Regelsysteme in Flugzeugen
US Government Reports ; Apr ; 1-53
1982
53 Seiten
Report
English
Aircraft Loss-Of-Control Recovery Using Nonlinear Smooth Feedback Regulators
British Library Conference Proceedings | 2011
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