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Results: 1-25/240

Authors: SINGH T
Citation: T. Singh, FUEL TIME OPTIMAL-CONTROL OF THE BENCHMARK PROBLEM/, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1225-1231

Authors: BOURMISTROV AS HILL RD RISEBOROUGH P
Citation: As. Bourmistrov et al., NONLINEAR CONTROL LAW FOR AERIAL TOWED TARGET, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1232-1238

Authors: SPARKS AG BERNSTEIN DS
Citation: Ag. Sparks et Ds. Bernstein, OPTIMAL TRADEOFF BETWEEN H-2 PERFORMANCE AND TRACKING ACCURACY IN SERVOCOMPENSATOR SYNTHESIS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1239-1243

Authors: SPARKS AG BERNSTEIN DS
Citation: Ag. Sparks et Ds. Bernstein, REAL STRUCTURED SINGULAR-VALUE SYNTHESIS USING THE SCALED POPOV CRITERION, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1244-1252

Authors: OCHI Y KANAI K
Citation: Y. Ochi et K. Kanai, POLE-PLACEMENT IN OPTIMAL REGULATOR BY CONTINUOUS POLE-SHIFTING, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1253-1258

Authors: HUMBLE WE PIERSON BL
Citation: We. Humble et Bl. Pierson, MAXIMUM-PAYLOAD TRAJECTORIES FOR A LASER-PROPELLED LAUNCH VEHICLE, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1259-1266

Authors: MARTELL CA LAWTON JA
Citation: Ca. Martell et Ja. Lawton, ADJOINT VARIABLE SOLUTIONS VIA AN AUXILIARY OPTIMIZATION PROBLEM, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1267-1272

Authors: IDAN M GOLAN OM GUELMAN M
Citation: M. Idan et al., OPTIMAL PLANAR INTERCEPTION WITH TERMINAL CONSTRAINTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1273-1279

Authors: NAPOLITANO MR NEPPACH C CASDORPH V NAYLOR S INNOCENTI M SILVESTRI G
Citation: Mr. Napolitano et al., NEURAL-NETWORK-BASED SCHEME FOR SENSOR FAILURE-DETECTION, IDENTIFICATION, AND ACCOMMODATION, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1280-1286

Authors: WEEKS CJ BOWERS MJ
Citation: Cj. Weeks et Mj. Bowers, ANALYTICAL MODELS OF DOPPLER DATA SIGNATURES, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1287-1291

Authors: TRANKLE TL BACHNER SD
Citation: Tl. Trankle et Sd. Bachner, IDENTIFICATION OF A NONLINEAR AERODYNAMIC MODEL OF THE F-14 AIRCRAFT, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1292-1297

Authors: PINSKY MA ESSARY B
Citation: Ma. Pinsky et B. Essary, RESONANCE CONTROL OF AIRCRAFT INSTABILITIES BY SMOOTH AND CONTINUOUS FEEDBACK, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1298-1304

Authors: PUIGSUARI J LONGUSKI JM TRAGESSER SG
Citation: J. Puigsuari et al., AEROCAPTURE WITH A FLEXIBLE TETHER, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1305-1312

Authors: HABLANI HB
Citation: Hb. Hablani, COMPARATIVE STABILITY ANALYSIS AND PERFORMANCE OF MAGNETIC CONTROLLERS FOR BIAS MOMENTUM SATELLITES, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1313-1320

Authors: HABLANI HB
Citation: Hb. Hablani, MAGNETIC PRECESSION AND PRODUCT-OF-INERTIA NUTATION DAMPING OF BIAS MOMENTUM SATELLITES, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1321-1328

Authors: TSUI R HALL CD
Citation: R. Tsui et Cd. Hall, RESONANCE CAPTURE IN UNBALANCED DUAL-SPIN SPACECRAFT, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1329-1335

Authors: AGRAWAL BN BANG H
Citation: Bn. Agrawal et H. Bang, ROBUST CLOSED-LOOP CONTROL DESIGN FOR SPACECRAFT SLEW MANEUVER USING THRUSTERS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1336-1344

Authors: LO SC CHEN YP
Citation: Sc. Lo et Yp. Chen, SMOOTH SLIDING-MODE CONTROL FOR SPACECRAFT ATTITUDE TRACKING MANEUVERS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1345-1349

Authors: VADALI SR KRISHNAN S
Citation: Sr. Vadali et S. Krishnan, SUBOPTIMAL COMMAND GENERATION FOR CONTROL MOMENT GYROSCOPES AND FEEDBACK-CONTROL OF SPACECRAFT, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1350-1354

Authors: HABLANI HB
Citation: Hb. Hablani, ROLL PITCH DETERMINATION WITH SCANNING HORIZON SENSORS - OBLATENESS AND ALTITUDE CORRECTIONS/, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1355-1364

Authors: FUJIKAWA SJ ZIMBELMAN DF
Citation: Sj. Fujikawa et Df. Zimbelman, SPACECRAFT ATTITUDE DETERMINATION BY KALMAN FILTERING OF GLOBAL POSITIONING SYSTEM SIGNALS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1365-1371

Authors: WIE B LU JB
Citation: B. Wie et Jb. Lu, FEEDBACK-CONTROL LOGIC FOR SPACECRAFT EIGENAXIS ROTATIONS UNDER SLEW RATE AND CONTROL CONSTRAINTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1372-1379

Authors: VADALI SR CARTER MT SINGH T ABHYANKAR NS
Citation: Sr. Vadali et al., NEAR-MINIMUM-TIME MANEUVERS OF LARGE STRUCTURES - THEORY AND EXPERIMENTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1380-1385

Authors: KONINGSTEIN R CANNON RH
Citation: R. Koningstein et Rh. Cannon, EXPERIMENTS WITH MODEL-SIMPLIFIED COMPUTED-TORQUE MANIPULATOR CONTROLLERS FOR FREE-FLYING ROBOTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1386-1391

Authors: TADIKONDA SSK
Citation: Ssk. Tadikonda, MODELING OF TRANSLATIONAL MOTION BETWEEN 2 FLEXIBLE BODIES CONNECTED VIA 3 POINTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1392-1397
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