APPLICATION OF THE PERFORMANCE OPERATOR TO AIRCRAFT AUTOMATIC CONTROL

[1] AHRENDT WR, 1947, AUTOMATIC REGULATION, V1

[2] Bode H. W., 1945, NETWORK ANAL FEEDBAC

[3] BROMBERG BG, 1947, THESIS MIT

[4] BROWN GS, 1940, BEHAVIOR DESIGN SERV

[5] DRAPER CS, 1940, ASME T JUL

[6] DURAND WF, 1943, AERODYNAMIC THEORY, V5

[7] EAGLE A, 1925, FOURIERS THEOREM HAR

[8] GARDNER MF, 1945, TRANSIENTS LINEAR SY, V1

[9] GUILLEMIN EA, 1935, COMMUNICATION NETWOR, V2

[10] Guillemin EA, 1935, COMMUNICATION NETWOR, V1

[1] AHRENDT WR, 1947, AUTOMATIC REGULATION, V1

[2] Bode H. W., 1945, NETWORK ANAL FEEDBAC

[3] BROMBERG BG, 1947, THESIS MIT

[4] BROWN GS, 1940, BEHAVIOR DESIGN SERV

[5] DRAPER CS, 1940, ASME T JUL

[6] DURAND WF, 1943, AERODYNAMIC THEORY, V5

[7] EAGLE A, 1925, FOURIERS THEOREM HAR

[8] GARDNER MF, 1945, TRANSIENTS LINEAR SY, V1

[9] GUILLEMIN EA, 1935, COMMUNICATION NETWOR, V2

[10] Guillemin EA, 1935, COMMUNICATION NETWOR, V1