DocumentCode :
312815
Title :
Supplemental control for robust flight cruise in turbulent time windows
Author :
Ashokkumar, C.R. ; Homaifar, A. ; Williams, Rolanda
Author_Institution :
Center for Aeros. Res., North Carolina A&T State Univ., Greensboro, NC, USA
Volume :
2
fYear :
1997
fDate :
4-6 Jun 1997
Firstpage :
1116
Abstract :
Turbulence during flight cruise is known to prevail over discrete time windows. The control surface deflections to recover ride quality at these time windows are important, specifically in high speed cruise vehicles. In this paper, we assume that the turbulence is measurable as an impulse of known intensity at a given time instant and, provide simple formulas for the supplemental control impulse minimizing its effect on ride quality. These thumb rules are particularly useful to evaluate the desired ride quality metrics, control magnitudes etc., at the time instances during which the flight cruise is felt with turbulence. In the high speed civil transport type of vehicles, these magnitudes are critical and may be discontinuous with respect to the nominal flight cruise
Keywords :
aircraft control; robust control; turbulence; control magnitudes; control surface deflections; high speed civil transport type vehicles; ride quality; robust flight cruise; supplemental control; turbulent time windows; Chromium; Frequency; Land vehicles; Measurement techniques; Optimal control; Road vehicles; Robust control; Thumb; Time measurement; Wheels;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
ISSN :
0743-1619
Print_ISBN :
0-7803-3832-4
Type :
conf
DOI :
10.1109/ACC.1997.609706
Filename :
609706
Link To Document :
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