Disturbance rejection for an aircraft flying in atmospheric disturbances

 
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1995 (EN)
Disturbance rejection for an aircraft flying in atmospheric disturbances (EN)

Skarpetis, MG (EN)

N/A (EN)

For an aircraft flying in atmospheric disturbances a static state feedback controller is designed. The design goal is that of rejecting the influence of a rotary gust disturbance to the vertical and forward velocity of the aircraft. The necessary and sufficient condition for this problem to have a solution is derived in terms of simple forms involving only the flight stability derivatives of the aircraft. The general analytical expression of the disturbance rejection controller matrix and the resulting closed, loop system, are derived in forms involving the aircraft parameters as well as arbitrary design parameters. The necessary and sufficient conditions for disturbance rejection with simultaneous stabilizability of the closed loop flight system are also established. © 1995 Kluwer Academic Publishers. (EN)

journalArticle

Stabilizability (EN)
Disturbance rejection (EN)
System stability (EN)
Wind effects (EN)
Control system synthesis (EN)
Vectors (EN)
Closed loop control systems (EN)
Feedback control (EN)
Aircraft (EN)
Velocity (EN)
Atmospheric disturbance (EN)

Εθνικό Μετσόβιο Πολυτεχνείο (EL)
National Technical University of Athens (EN)

Dynamics and Control (EN)

English

1995


Kluwer Academic Publishers (EN)



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