FLIGHT CONTROL DESIGN USING NON-LINEAR INVERSE DYNAMICS

[1] ASSEO SJ, 1973, AIAA J AIRCRAFT, V10, P739

[2] EHRENSTROM WA, 1983, THESIS PRINCETON U

[3] Etkin B., 1972, DYNAMICS ATMOSPHERIC, P134

[4] DECOUPLING IN DESIGN AND SYNTHESIS OF MULTIVARIABLE CONTROL SYSTEMS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1967, AC12 (06) : 651 - +

[5] FRATTER C, 1982, THESIS PRINCETON U

[6] FREUND E, 1975, INT J CONTROL, V21, P443, DOI 10.1080/00207177508922001

[7] DECOUPLING AND POLE ASSIGNMENT IN NONLINEAR-SYSTEMS [J]. ELECTRONICS LETTERS, 1973, 9 (16) : 373 - 374

[8] LANE SH, 1987, 1987 P AM CONTR C MI, P1224

[9] MENON PKA, 1985, AIAA GUIDANCE CONTRO

[10] APPLICATION OF NONLINEAR TRANSFORMATIONS TO AUTOMATIC FLIGHT CONTROL [J]. AUTOMATICA, 1984, 20 (01) : 103 - 107

[1] ASSEO SJ, 1973, AIAA J AIRCRAFT, V10, P739

[2] EHRENSTROM WA, 1983, THESIS PRINCETON U

[3] Etkin B., 1972, DYNAMICS ATMOSPHERIC, P134

[4] DECOUPLING IN DESIGN AND SYNTHESIS OF MULTIVARIABLE CONTROL SYSTEMS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1967, AC12 (06) : 651 - +

[5] FRATTER C, 1982, THESIS PRINCETON U

[6] FREUND E, 1975, INT J CONTROL, V21, P443, DOI 10.1080/00207177508922001

[7] DECOUPLING AND POLE ASSIGNMENT IN NONLINEAR-SYSTEMS [J]. ELECTRONICS LETTERS, 1973, 9 (16) : 373 - 374

[8] LANE SH, 1987, 1987 P AM CONTR C MI, P1224

[9] MENON PKA, 1985, AIAA GUIDANCE CONTRO

[10] APPLICATION OF NONLINEAR TRANSFORMATIONS TO AUTOMATIC FLIGHT CONTROL [J]. AUTOMATICA, 1984, 20 (01) : 103 - 107