DocumentCode
3184186
Title
The UTA autonomous aerial vehicle-automatic control
Author
Black, Kliffton M. ; Smith, Jeffrey O. ; Roberts, Richard A.
Author_Institution
Texas Univ., Arlington, TX, USA
fYear
1992
fDate
18-22 May 1992
Firstpage
489
Abstract
Some preliminary results on the design and implementation of robust automatic controls for the University of Texas at Arlington autonomous VTOL (vertical takeoff and landing) prototype are presented. Both stability augmentation and navigational issues are addressed. Since the use of inexpensive sensors and actuators has resulted in a relatively large degree of uncertainty about the system model, a robust controller is required. The authors demonstrate the mixed H 2/H Ω-optimal design methodology used to obtain the automatic controllers for this aircraft. The technique used is a loop transfer recovery procedure which has been generalized by the removal of an assumption constraining a design variable
Keywords
aircraft control; control system synthesis; multivariable control systems; navigation; optimal control; stability; Arlington autonomous VTOL; H2/HΩ-optimal design; UTA autonomous aerial vehicle; actuators; aircraft control; automatic control; loop transfer recovery; prototype; robust automatic controls; robust controller; sensors; stability augmentation; system model; uncertainty; vertical takeoff and landing; Actuators; Aircraft; Automatic control; Design methodology; Navigation; Prototypes; Robust control; Sensor systems; Stability; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1992. NAECON 1992., Proceedings of the IEEE 1992 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0652-X
Type
conf
DOI
10.1109/NAECON.1992.220527
Filename
220527
Link To Document