DESIGN OF OPTIMAL AND SUBOPTIMAL STABILITY AUGMENTATION SYSTEMS

[1] OPTIMIZATION OF THE FLIGHT-CONTROL, AIRFRAME SYSTEM [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (03): : 197 - 218

[2] ASHKENAS IL, 1965, AIAA65314 PAP

[3] APPLICATIONS OF OPTIMAL CONTROL THEORY IN AEROSPACE ENGINEERING [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (05) : 545 - +

[4] APPLICATION OF DYNAMIC PROGRAMMING TO DESIGN OF INVARIANT AUTO-STABILISERS [J]. JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, 1966, 70 (664): : 469 - +

[5] Kalman Rudolph E., 1960, B SOC MATH, V5, P102

[6] Merriam C. W., 1959, J FRANKLIN I, V267, P267, DOI 10.1016/0016-0032(59)90149-8

[7] Penrose R., 1955, MATH PROC CAMBRIDGE, V51, P406, DOI [10.1017/S0305004100030401, DOI 10.1017/S0305004100030401]

[8] TYLER JS, 1964, IEEE T, VAC 9, P485

[9] YORE EE, 1968, J AM COLL CARDIOL, P327

[10] 1952, AE644II US BUR AER N

[1] OPTIMIZATION OF THE FLIGHT-CONTROL, AIRFRAME SYSTEM [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (03): : 197 - 218

[2] ASHKENAS IL, 1965, AIAA65314 PAP

[3] APPLICATIONS OF OPTIMAL CONTROL THEORY IN AEROSPACE ENGINEERING [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (05) : 545 - +

[4] APPLICATION OF DYNAMIC PROGRAMMING TO DESIGN OF INVARIANT AUTO-STABILISERS [J]. JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, 1966, 70 (664): : 469 - +

[5] Kalman Rudolph E., 1960, B SOC MATH, V5, P102

[6] Merriam C. W., 1959, J FRANKLIN I, V267, P267, DOI 10.1016/0016-0032(59)90149-8

[7] Penrose R., 1955, MATH PROC CAMBRIDGE, V51, P406, DOI [10.1017/S0305004100030401, DOI 10.1017/S0305004100030401]

[8] TYLER JS, 1964, IEEE T, VAC 9, P485

[9] YORE EE, 1968, J AM COLL CARDIOL, P327

[10] 1952, AE644II US BUR AER N