AAAAAA

   
Results: 1-13 |
Results: 13
NONLINEAR SIMULATION OF A MODIFIED F-16 WITH FULL-ENVELOPE CONTROL LAWS
Authors: REIGELSPERGER WC BANDA SS
Citation: Wc. Reigelsperger et Ss. Banda, NONLINEAR SIMULATION OF A MODIFIED F-16 WITH FULL-ENVELOPE CONTROL LAWS, Control engineering practice, 6(3), 1998, pp. 309-320
ROBUST-CONTROL LAW DESIGN FOR LATERAL-DIRECTIONAL MODES OF AN F-16 MATV USING MU-SYNTHESIS AND DYNAMIC INVERSION/
Authors: REIGELSPERGER WC HAMMETT KD BANDA SS
Citation: Wc. Reigelsperger et al., ROBUST-CONTROL LAW DESIGN FOR LATERAL-DIRECTIONAL MODES OF AN F-16 MATV USING MU-SYNTHESIS AND DYNAMIC INVERSION/, International journal of robust and nonlinear control, 7(8), 1997, pp. 777-795
REDUCED-ORDER ROBUST COMPENSATOR DESIGN WITH REAL PARAMETER UNCERTAINTY
Authors: YEH HH HSU CS BANDA SS RAWSON JL
Citation: Hh. Yeh et al., REDUCED-ORDER ROBUST COMPENSATOR DESIGN WITH REAL PARAMETER UNCERTAINTY, International journal of robust and nonlinear control, 7(12), 1997, pp. 1029-1045
AN ANALYSIS OF THE DESTABILIZING EFFECT OF DAISY CHAINED RATE-LIMITEDACTUATORS
Authors: BERG JM HAMMETT KD SCHWARTZ CA BANDA SS
Citation: Jm. Berg et al., AN ANALYSIS OF THE DESTABILIZING EFFECT OF DAISY CHAINED RATE-LIMITEDACTUATORS, IEEE transactions on control systems technology, 4(2), 1996, pp. 171-176
OBSERVER-BASED COMPENSATORS FOR FIXED-ORDER H-INFINITY CONTROL
Authors: JUANG JC YEH HH BANDA SS
Citation: Jc. Juang et al., OBSERVER-BASED COMPENSATORS FOR FIXED-ORDER H-INFINITY CONTROL, International Journal of Control, 64(3), 1996, pp. 441-461
NONLINEAR OPTIMIZATION-BASED DESIGN OF RAM VELOCITY PROFILES FOR ISOTHERMAL FORGING
Authors: BERG JM ADAMS RJ MALAS JC BANDA SS
Citation: Jm. Berg et al., NONLINEAR OPTIMIZATION-BASED DESIGN OF RAM VELOCITY PROFILES FOR ISOTHERMAL FORGING, IEEE transactions on control systems technology, 3(3), 1995, pp. 269-278
DESIGN OF NONLINEAR CONTROL LAWS FOR HIGH-ANGLE-OF-ATTACK FLIGHT
Authors: ADAMS RJ BUFFINGTON JM BANDA SS
Citation: Rj. Adams et al., DESIGN OF NONLINEAR CONTROL LAWS FOR HIGH-ANGLE-OF-ATTACK FLIGHT, Journal of guidance, control, and dynamics, 17(4), 1994, pp. 737-746
IMPLEMENTATION OF A FULL-ENVELOPE CONTROLLER FOR A HIGH-PERFORMANCE AIRCRAFT
Authors: ADAMS RJ BUFFINGTON JM BANDA SS
Citation: Rj. Adams et al., IMPLEMENTATION OF A FULL-ENVELOPE CONTROLLER FOR A HIGH-PERFORMANCE AIRCRAFT, Journal of guidance, control, and dynamics, 17(3), 1994, pp. 578-583
REDUCED-ORDER H-INFINITY COMPENSATOR DESIGN FOR AN AIRCRAFT CONTROL PROBLEM
Authors: OSBORNE RC ADAMS RJ HSU CS BANDA SS
Citation: Rc. Osborne et al., REDUCED-ORDER H-INFINITY COMPENSATOR DESIGN FOR AN AIRCRAFT CONTROL PROBLEM, Journal of guidance, control, and dynamics, 17(2), 1994, pp. 341-345
H-INFINITY COMPENSATOR DESIGN WITH MINIMAL ORDER OBSERVERS
Authors: HSU CS YU XG YEH HH BANDA SS
Citation: Cs. Hsu et al., H-INFINITY COMPENSATOR DESIGN WITH MINIMAL ORDER OBSERVERS, IEEE transactions on automatic control, 39(8), 1994, pp. 1679-1681
ROBUST LONGITUDINAL AXIS FLIGHT CONTROL FOR AN AIRCRAFT WITH THRUST VECTORING
Authors: BUFFINGTON JM SPARKS AG BANDA SS
Citation: Jm. Buffington et al., ROBUST LONGITUDINAL AXIS FLIGHT CONTROL FOR AN AIRCRAFT WITH THRUST VECTORING, Automatica, 30(10), 1994, pp. 1527-1540
APPLICATION OF STRUCTURED SINGULAR-VALUE SYNTHESIS TO A FIGHTER AIRCRAFT
Authors: SPARKS A BANDA SS
Citation: A. Sparks et Ss. Banda, APPLICATION OF STRUCTURED SINGULAR-VALUE SYNTHESIS TO A FIGHTER AIRCRAFT, Journal of guidance, control, and dynamics, 16(5), 1993, pp. 940-947
FULL ENVELOPE MULTIVARIABLE CONTROL LAW SYNTHESIS FOR A HIGH-PERFORMANCE TEST AIRCRAFT
Authors: ADAMS RJ SPARKS A BANDA SS
Citation: Rj. Adams et al., FULL ENVELOPE MULTIVARIABLE CONTROL LAW SYNTHESIS FOR A HIGH-PERFORMANCE TEST AIRCRAFT, Journal of guidance, control, and dynamics, 16(5), 1993, pp. 948-955
Risultati: 1-13 |