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Authors: NEWMAN B SCHMIDT DK
Citation: B. Newman et Dk. Schmidt, AEROELASTIC VEHICLE MULTIVARIABLE CONTROL SYNTHESIS WITH ANALYTICAL ROBUSTNESS EVALUATION, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1145-1153

Authors: SEYWALD H CLIFF EM
Citation: H. Seywald et Em. Cliff, NEIGHBORING OPTIMAL-CONTROL BASED FEEDBACK LAW FOR THE ADVANCED LAUNCH SYSTEM, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1154-1162

Authors: GROCOTT S HOW J MILLER D MACMARTIN D LIU K
Citation: S. Grocott et al., ROBUST-CONTROL DESIGN AND IMPLEMENTATION ON THE MIDDECK ACTIVE CONTROL EXPERIMENT, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1163-1170

Authors: LI FY BAINUM PM
Citation: Fy. Li et Pm. Bainum, ANALYTIC TIME-OPTIMAL CONTROL SYNTHESIS OF 4TH-ORDER SYSTEM AND MANEUVERS OF FLEXIBLE STRUCTURES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1171-1178

Authors: GAWRONSKI W MELLSTROM JA
Citation: W. Gawronski et Ja. Mellstrom, ANTENNA SERVO DESIGN FOR TRACKING LOW-EARTH-ORBITING SATELLITES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1179-1184

Authors: SCHEEL WA CONWAY BA
Citation: Wa. Scheel et Ba. Conway, OPTIMIZATION OF VERY-LOW-THRUST, MANY-REVOLUTION SPACECRAFT TRAJECTORIES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1185-1192

Authors: RYAN GW DOWNING DR
Citation: Gw. Ryan et Dr. Downing, FUNCTIONAL AGILITY METRICS AND OPTIMAL TRAJECTORY ANALYSIS, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1193-1197

Authors: TRILLER MJ KAMMER DC
Citation: Mj. Triller et Dc. Kammer, CONTROLLABILITY AND OBSERVABILITY MEASURES FOR CRAIG-BAMPTON SUBSTRUCTURE REPRESENTATIONS, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1198-1204

Authors: PAO LY
Citation: Ly. Pao, MULTISENSOR MULTITARGET MIXTURE REDUCTION ALGORITHMS FOR TRACKING, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1205-1211

Authors: LEW JS KEEL LH JUANG JN
Citation: Js. Lew et al., QUANTIFICATION OF PARAMETRIC UNCERTAINTY VIA AN INTERVAL MODEL, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1212-1218

Authors: NEWMAN B SCHMIDT DK
Citation: B. Newman et Dk. Schmidt, MULTIVARIABLE STABILITY AND ROBUSTNESS OF SEQUENTIALLY DESIGNED FEEDBACK-SYSTEMS, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1219-1227

Authors: DURHAM WC LUTZE FH MASON W
Citation: Wc. Durham et al., KINEMATICS AND AERODYNAMICS OF VELOCITY VECTOR ROLL, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1228-1233

Authors: VISSER HG
Citation: Hg. Visser, OPTIMAL LATERAL-ESCAPE MANEUVERS FOR MICROBURST ENCOUNTERS DURING FINAL APPROACH, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1234-1240

Authors: JENG YF SWAIM RL
Citation: Yf. Jeng et Rl. Swaim, MULTIAXIS PILOT RATINGS FOR DAMAGED AIRCRAFT, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1241-1244

Authors: TAKAHASHI MD
Citation: Md. Takahashi, H-INFINITY HELICOPTER FLIGHT CONTROL LAW DESIGN WITH AND WITHOUT ROTOR STATE-FEEDBACK, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1245-1251

Authors: CHENG VHL LAM T
Citation: Vhl. Cheng et T. Lam, AUTOMATIC GUIDANCE AND CONTROL FOR HELICOPTER OBSTACLE AVOIDANCE, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1252-1259

Authors: VU P BIEZAD DJ
Citation: P. Vu et Dj. Biezad, DIRECT-LIFT DESIGN STRATEGY FOR LONGITUDINAL CONTROL OF HYPERSONIC AIRCRAFT, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1260-1266

Authors: MASON GS BERG MC
Citation: Gs. Mason et Mc. Berg, MULTIRATE FLUTTER SUPPRESSION SYSTEM-DESIGN FOR A MODEL WING, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1267-1274

Authors: PIERSON BL KLUEVER CA
Citation: Bl. Pierson et Ca. Kluever, 3-STAGE APPROACH TO OPTIMAL LOW-THRUST EARTH-MOON TRAJECTORIES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1275-1282

Authors: UDOMKESMALEE S ALEXANDER JW TOLIVAR AF
Citation: S. Udomkesmalee et al., STOCHASTIC STAR IDENTIFICATION, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1283-1286

Authors: CRISTI R BURL J RUSSO N
Citation: R. Cristi et al., ADAPTIVE QUATERNION FEEDBACK-REGULATION FOR EIGENAXIS ROTATIONS, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1287-1291

Authors: FUJII HA ANAZAWA S
Citation: Ha. Fujii et S. Anazawa, DEPLOYMENT RETRIEVAL CONTROL OF TETHERED SUBSATELLITE THROUGH AN OPTIMAL PATH, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1292-1298

Authors: NEWMAN B SCHMIDT DK
Citation: B. Newman et Dk. Schmidt, TRUNCATION AND RESIDUALIZATION WITH WEIGHTED BALANCED COORDINATES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1299-1307

Authors: CHAVEZ FR SCHMIDT DK
Citation: Fr. Chavez et Dk. Schmidt, ANALYTICAL AEROPROPULSIVE AEROELASTIC HYPERSONIC VEHICLE MODEL WITH DYNAMIC ANALYSIS, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1308-1319

Authors: SUGIYAMA N
Citation: N. Sugiyama, DERIVATION OF SYSTEM MATRICES FROM NONLINEAR DYNAMIC SIMULATION OF JET ENGINES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1320-1326
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