A gas-turbine aero-engine speed-control system has been investigated on an analogue computer to determine the possibility of using a model reference adaptive control device to maintain constant dynamic behaviour of engine speed irrespective of altitude and aircraft forward speed.
Design analysis of model reference adaptive control systems applied to a gasturbine aircraft engine
Proceedings of the IEE ; 115 , 3 ; 460-466
1968
7 Seiten, 6 Bilder, 3 Tabellen, 13 Quellen
Article (Journal)
English
ANALOGRECHNER , ANTRIEB , FLUGREGELUNG , FLUGZEUG , GASTURBINE , MODELL , REGELUNG , SIMULATION
Design of model reference adaptive control for unstable aircraft
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