APPLICATION OF PRECOMPUTED CONTROL LAWS IN A RECONFIGURABLE AIRCRAFT FLIGHT CONTROL-SYSTEM

[1] BROUSSARD J, 1984, ICS TM84027

[2] DESIGN AND FLIGHT TESTING OF A DIGITAL OPTIMAL-CONTROL GENERAL-AVIATION AUTOPILOT [J]. AUTOMATICA, 1985, 21 (01) : 23 - 34

[3] CAGLAYAN A, 1987, AFWAL TR873024 AIR F

[4] CHANDLER PR, 1984, SELF REPAIRING FLIGH

[5] HALYO N, 1983, ICS TM83011

[6] HALYO N, 1983, 1ST P ANN AIRCR CONT

[7] HOWELL W, 1983, AUG P AIAA GUID CONT

[8] ROBUSTNESS RESULTS IN LINEAR-QUADRATIC GAUSSIAN BASED MULTIVARIABLE CONTROL DESIGNS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1981, 26 (01) : 75 - 92

[9] LOOZE D, 1985, NASA CR172489

[10] Looze D. P., 1985, IEEE Control Systems Magazine, V5, P16, DOI 10.1109/MCS.1985.1104940

[1] BROUSSARD J, 1984, ICS TM84027

[2] DESIGN AND FLIGHT TESTING OF A DIGITAL OPTIMAL-CONTROL GENERAL-AVIATION AUTOPILOT [J]. AUTOMATICA, 1985, 21 (01) : 23 - 34

[3] CAGLAYAN A, 1987, AFWAL TR873024 AIR F

[4] CHANDLER PR, 1984, SELF REPAIRING FLIGH

[5] HALYO N, 1983, ICS TM83011

[6] HALYO N, 1983, 1ST P ANN AIRCR CONT

[7] HOWELL W, 1983, AUG P AIAA GUID CONT

[8] ROBUSTNESS RESULTS IN LINEAR-QUADRATIC GAUSSIAN BASED MULTIVARIABLE CONTROL DESIGNS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1981, 26 (01) : 75 - 92

[9] LOOZE D, 1985, NASA CR172489

[10] Looze D. P., 1985, IEEE Control Systems Magazine, V5, P16, DOI 10.1109/MCS.1985.1104940