Citation: Ja. Franklin et Sa. Engelland, DESIGN AND PILOTED SIMULATION OF INTEGRATED FLIGHT PROPULSION CONTROLS FOR STOVL AIRCRAFT, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 993-998
Citation: Mr. Napolitano et al., AIRCRAFT FAILURE-DETECTION AND IDENTIFICATION USING NEURAL NETWORKS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 999-1009
Citation: Ss. Mulgund et Rf. Stengel, OPTIMAL RECOVERY FROM MICROBURST WIND SHEAR, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1010-1017
Citation: Dj. Linse et Rf. Stengel, IDENTIFICATION OF AERODYNAMIC COEFFICIENTS USING COMPUTATIONAL NEURALNETWORKS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1018-1025
Citation: Jj. Burken, FLIGHT-DETERMINED MULTIVARIABLE STABILITY ANALYSIS AND COMPARISON OF A CONTROL-SYSTEM, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1026-1031
Citation: Rk. Yedavalli, FLIGHT CONTROL APPLICATION OF NEW STABILITY ROBUSTNESS BOUNDS FOR LINEAR UNCERTAIN SYSTEMS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1032-1037
Citation: Rw. Powell et Rd. Braun, 6-DEGREE-OF-FREEDOM GUIDANCE AND CONTROL ANALYSIS OF MARS AEROCAPTURE, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1038-1044
Citation: V. Coverstonecarroll et Je. Prussing, OPTIMAL COOPERATIVE POWER-LIMITED RENDEZVOUS BETWEEN NEIGHBORING CIRCULAR ORBITS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1045-1054
Citation: S. Kawase, DIFFERENTIAL ANGLE TRACKING FOR CLOSE GEOSTATIONARY SATELLITES, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1055-1060
Citation: T. Singh et Sr. Vadali, INPUT-SHAPED CONTROL OF 3-DIMENSIONAL MANEUVERS OF FLEXIBLE SPACECRAFT, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1061-1068
Citation: B. Wie et al., CLASSICAL AND ROBUST H-INFINITY CONTROL REDESIGN FOR THE HUBBLE-SPACE-TELESCOPE, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1069-1077
Citation: Me. Pittelkau, OPTIMAL PERIODIC CONTROL FOR SPACECRAFT POINTING AND ATTITUDE DETERMINATION, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1078-1084
Citation: E. Netzer et Tr. Kane, DEPLOYMENT AND RETRIEVAL OPTIMIZATION OF A TETHERED SATELLITE SYSTEM, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1085-1091
Citation: Ak. Banerjee, BLOCK-DIAGONAL EQUATIONS FOR MULTIBODY ELASTODYNAMICS WITH GEOMETRIC STIFFNESS AND CONSTRAINTS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1092-1100
Citation: Ay. Lee, COMPONENT MODES DAMPING ASSIGNMENT METHODOLOGY FOR ARTICULATED, MULTIFLEXIBLE BODY STRUCTURES, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1101-1108
Citation: Yj. Lee et Jl. Speyer, APPLICATION OF A PERIODIC LATTICE FILTER FOR IDENTIFYING FLEXIBLE STRUCTURES, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1109-1117
Citation: Lg. Horta et al., DISCRETE-TIME MODEL-REDUCTION IN LIMITED FREQUENCY RANGES, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1125-1130
Citation: Js. Yang, H-INFINITY-ROBUST CONTROL DESIGN FOR LINEAR FEEDBACK-SYSTEMS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1131-1137
Citation: Dp. Giesy et Kb. Lim, H-INFINITY NORM SENSITIVITY FORMULA WITH CONTROL-SYSTEM DESIGN APPLICATIONS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1138-1145
Citation: K. Matsuda et H. Fujii, H-INFINITY OPTIMIZED WAVE-ABSORBING CONTROL - ANALYTICAL AND EXPERIMENTAL RESULTS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1146-1153
Citation: E. Nissim, ORDER REDUCTION OF LINEAR-QUADRATIC-GAUSSIAN-DESIGNED CONTROLLERS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1154-1161
Citation: L. Silverberg et Jl. Meyer, FUEL-OPTIMAL SLEWING OF AN EXPERIMENTAL HINGED-FREE BEAM, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1162-1168
Citation: A. Deluca et B. Siciliano, INVERSION-BASED NONLINEAR CONTROL OF ROBOT ARMS WITH FLEXIBLE LINKS, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1169-1176
Citation: K. Xu et al., CONTROL OF A STRUCTURE WITH 2 CLOSELY SPACED FREQUENCIES, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1177-1178