DocumentCode
490122
Title
A Full-Authority 4D Guidance Algorithm for Conventional Aircraft
Author
Stiharu-Alexe, Ilie ; Stiharu-Alexe, Carmen
Author_Institution
Assistant Professor in Aeronautics, Laboratoire d´Automatique de Grenoble, ENSIEG, B.P. 46, 38402 Saint Martin d´Heres, FRANCE
fYear
1993
fDate
2-4 June 1993
Firstpage
420
Lastpage
424
Abstract
A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical solution to inverting the slow time-scale dynamics is found through the Inverse Kinematics Problem (IKP). The algorithm´s performance is evaluated in the terms of the tracking error.
Keywords
Aerodynamics; Aircraft; Attitude control; Control systems; Elevators; Error correction; Feedback control; Force control; Iron; Neodymium;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1993
Conference_Location
San Francisco, CA, USA
Print_ISBN
0-7803-0860-3
Type
conf
Filename
4792887
Link To Document