DocumentCode
393844
Title
Flight controller design taking account of control anticipation parameter
Author
Tokutake, Hiroshi ; Itoh, Eri
Author_Institution
Dept. of Aerosp. Eng., Osaka Prefecture Univ., Sakai, Japan
Volume
3
fYear
2002
fDate
5-7 Aug. 2002
Firstpage
1826
Abstract
The controller design method taking account of flying quality is proposed. It is assumed that pilot determines flying quality by control anticipation parameter (CAP). CAP condition is formulated in LMI forms and they are introduced into controller design. When the LMIs have solutions, flying quality of closed-loop system is guaranteed. Flying quality condition is combined with robust stability condition and verified by numerical example.
Keywords
aerospace control; closed loop systems; feedback; linear matrix inequalities; matrix algebra; robust control; stability; LMI forms; closed-loop system; control anticipation parameter; flight controller design; robust stability; Acceleration; Aerospace control; Design methodology; Elevators; Equations; Frequency; Motion control; Polynomials; Robust stability; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE 2002. Proceedings of the 41st SICE Annual Conference
Print_ISBN
0-7803-7631-5
Type
conf
DOI
10.1109/SICE.2002.1196598
Filename
1196598
Link To Document