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
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;
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA