DocumentCode
486586
Title
Time Scale Analysis of a Digital Flight Control System
Author
Naidu, D.S. ; Price, D.B.
Author_Institution
NASA Langley Research Center, Hampton, VA 23665
fYear
1986
fDate
18-20 June 1986
Firstpage
509
Lastpage
510
Abstract
In this paper, we consider the fifth order discrete model of an aircraft (longitudinal) control system which possesses three slow (velocity, pitch angle and altitude) and two fast (angle of attack and pitch angular velocity) modes and exhibits a two-time scale property. Using the recent results of the time scale analysis of discrete control systems, the high-order discrete model is decoupled into low-order slow and fast subsystems. The results of the decoupled system are found to be in excellent agreement with those of the original system.
Keywords
Aerospace control; Aerospace safety; Aircraft; Angular velocity; Angular velocity control; Bismuth; Control system analysis; Control system synthesis; NASA; Riccati equations;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1986
Conference_Location
Seattle, WA, USA
Type
conf
Filename
4788993
Link To Document