DocumentCode
3079616
Title
Aircraft control in a downburst on takeoff and landing
Author
Zhao, Yiyuan ; Bryson, A.E.
Author_Institution
Minnesota Univ., Minneapolis, MN, USA
fYear
1990
fDate
5-7 Dec 1990
Firstpage
753
Abstract
Dynamic optimization and feedback control system design techniques are used to determine proper guidance laws for aircraft in the presence of downbursts, and insensitivity to downburst structures is emphasized. Avoidance is the best policy. If an inadvertent encounter occurs when the aircraft is already close to or even in the downburst, the pilot should concentrate on vertical flight, unless he is sure which direction to turn for winds of less intensity. If such an encounter happens on takeoff, maximum thrust should be aggressively and a lower climb rate or even descending flight is recommended. Similar strategy is applicable for abort landing. If an encounter happens on landing and encounter height is low, landing should proceed. It is recommended that the nominal horizontal and vertical velocities w.r.t. the ground should be maintained, subject to a minimum airspeed constraint. A landing control logic is designed to accomplish this
Keywords
aircraft control; attitude control; control system synthesis; feedback; optimisation; aircraft control; climb rate; downburst; dynamic optimisation; feedback; landing; takeoff; thrust; Aerospace control; Aerospace simulation; Aircraft; Design optimization; Equations; Feedback control; Logic design; Meteorology;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
Conference_Location
Honolulu, HI
Type
conf
DOI
10.1109/CDC.1990.203688
Filename
203688
Link To Document