The design of the control of an aircraft encountering windshear after takeoff is treated as a problem of stabilizing the climb rate about a desired value of the climb rate. The resulting controller is a feedback one utilizing only climb rate information. Its robustness namely windshear structure and intensity is illustrated via simulations employing four different windshear models. The simulations were carried out for the Boeing 727 aircraft.
Aircraft control under conditions of windshear
Die Flugzeugsteuerung nach dem Start beim Auftreten von Scherwinden
1990
6 Seiten, 17 Quellen
Conference paper
English
Aircraft flight characteristics in conditions of windshear and icing
Online Contents | 2007
|Variable Structure Control for Aircraft in Windshear Field
British Library Conference Proceedings | 1995
|Lidar windshear detection for commercial aircraft
NTRS | 1991
|H[infinity] control for aircraft take off in windshear
TIBKAT | 1995
|Windshear During Heavy Showers Windshear Bij Zware Buien
NTIS | 1980
|