Design and simulation of a parameter varying controller for a fighter aircraft

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Gunnarsson, Karin Ståhl ^a   Jacobsen, Jan Ole ^a  

^a SAAB AB   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT MODELS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; LINEAR MATRIX INEQUALITIES; LINEAR TRANSFORMATIONS; MACH NUMBER; MATHEMATICAL TRANSFORMATIONS; SUPERSONIC AIRCRAFT;

CANARD CONFIGURATION; DESIGN AND SIMULATION; DYNAMICS UNCERTAINTIES; LINEAR FRACTIONAL TRANSFORMATIONS; LINEAR PARAMETER VARYING; LINEAR-PARAMETER VARYING CONTROLLERS; LONGITUDINAL DYNAMICS; NONLINEAR SIMULATIONS;

CONTROLLERS;

EID: 85087189555     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4105     Document Type: Conference Paper

References (4)

1. P. Apkarian, On the Discretization of LMI-synthesized Linear Parameter-vary ing Controllers, Automatica, Vol. 33, No. 4, pp-655-661, 1997.
2. J-M Biannic, P. Apkarian, W. Garrard, Parameter Varying Control of a High Performance Aircraft, AIAA Guidance navigation and Control Conference, July 29-31, 1996
3. A. Helmersson, Methods for Robust Gain Scheduling. PhD These, Department of Electrical Engineering, Linkoping University, Sweden. 1995.
4. DJ. Leith and W.E. Leithead, Survey of gainscheduling analysis and design, Int. J. Control. 2000. Vol. 73, No. 11, pp. 1001-1025.