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Results: 1-25/179

Authors: Jalili, N Olgac, N
Citation: N. Jalili et N. Olgac, Identification and retuning of optimum delayed feedback vibration absorber, J GUID CON, 23(6), 2000, pp. 961-970

Authors: Roger, AB McInnes, CR
Citation: Ab. Roger et Cr. Mcinnes, Safety constrained free-flyer path planning at the International Space Station, J GUID CON, 23(6), 2000, pp. 971-979

Authors: Ford, JJ Evans, ME
Citation: Jj. Ford et Me. Evans, Online estimation of Allan variance parameters, J GUID CON, 23(6), 2000, pp. 980-987

Authors: Leith, DJ Leithead, WE
Citation: Dj. Leith et We. Leithead, Gain-scheduled control: Relaxing slow variation requirements by velocity-based design, J GUID CON, 23(6), 2000, pp. 988-1000

Authors: Yaesh, I Shaked, U
Citation: I. Yaesh et U. Shaked, Robust H-infinity deconvolution and its application to fault detection, J GUID CON, 23(6), 2000, pp. 1001-1012

Authors: Shtessel, Y Hall, C Jackson, M
Citation: Y. Shtessel et al., Reusable launch vehicle control in multiple-time-scale sliding modes, J GUID CON, 23(6), 2000, pp. 1013-1020

Authors: Korgul, A
Citation: A. Korgul, Novel method for identification of aircraft trajectories in three-dimensional space, J GUID CON, 23(6), 2000, pp. 1021-1029

Authors: Bernelli-Zazzera, F Mantegazza, P Mazzoni, G Rendina, M
Citation: F. Bernelli-zazzera et al., Active flutter suppression using recurrent neural networks, J GUID CON, 23(6), 2000, pp. 1030-1036

Authors: Chen, ZY Voulgaris, PG
Citation: Zy. Chen et Pg. Voulgaris, Decentralized design for integrated flight/propulsion control of aircraft, J GUID CON, 23(6), 2000, pp. 1037-1044

Authors: Ukpai, UI Nwokah, ODI Boje, E
Citation: Ui. Ukpai et al., Quantitative cross-feed and feedback design of helicopter in near hover flight, J GUID CON, 23(6), 2000, pp. 1045-1054

Authors: Sultan, C Corless, M Skelton, RE
Citation: C. Sultan et al., Tensegrity flight simulator, J GUID CON, 23(6), 2000, pp. 1055-1064

Authors: Markley, FL Reynolds, RG
Citation: Fl. Markley et Rg. Reynolds, Analytic steady-state accuracy of a spacecraft attitude estimator, J GUID CON, 23(6), 2000, pp. 1065-1067

Authors: Song, TL Collins, EG
Citation: Tl. Song et Eg. Collins, Robust H-2 estimation with application to robust fault detection, J GUID CON, 23(6), 2000, pp. 1067-1071

Authors: Krempasky, JJ
Citation: Jj. Krempasky, Closed-form solution of seventh-order navigation system for unaided flyout, J GUID CON, 23(6), 2000, pp. 1072-1076

Authors: McInnes, CR
Citation: Cr. Mcinnes, Payload mass fractions for minimum-time trajectories of flat and compound solar sails, J GUID CON, 23(6), 2000, pp. 1076-1078

Authors: Blanksby, C Trivailo, P
Citation: C. Blanksby et P. Trivailo, Collision dynamics for space tethers, J GUID CON, 23(6), 2000, pp. 1078-1081

Authors: Frost, G Costello, M
Citation: G. Frost et M. Costello, Two projectiles connected by a flexible tether dropped in the atmosphere, J GUID CON, 23(6), 2000, pp. 1081-1085

Authors: Bar-Itzhack, IY
Citation: Iy. Bar-itzhack, New method for extracting the quaternion from a rotation matrix, J GUID CON, 23(6), 2000, pp. 1085-1087

Authors: Lisano, ME
Citation: Me. Lisano, Comment on "new, guaranteed positive time update for the two-step optimal estimator", J GUID CON, 23(6), 2000, pp. 1088-1090

Authors: Kasdin, NJ
Citation: Nj. Kasdin, Comment on "new, guaranteed positive time update for the two-step optimal estimator" - Reply by the author to M. Lisano, J GUID CON, 23(6), 2000, pp. 1090-1090

Authors: Mukhopadhyay, V
Citation: V. Mukhopadhyay, Benchmark active control technology special section: Part II, J GUID CON, 23(6), 2000, pp. 1093-1093

Authors: Bartels, RE Schuster, DM
Citation: Re. Bartels et Dm. Schuster, Comparison of two Navier-Stokes methods with benchmark active control technology experiments, J GUID CON, 23(6), 2000, pp. 1094-1099

Authors: Scott, RC Pado, LE
Citation: Rc. Scott et Le. Pado, Active control of wind-tunnel model aeroelastic response using neural networks, J GUID CON, 23(6), 2000, pp. 1100-1108

Authors: Xing, WH Singh, SN
Citation: Wh. Xing et Sn. Singh, Adaptive output feedback control of a nonlinear aeroelastic structure, J GUID CON, 23(6), 2000, pp. 1109-1116

Authors: Guillot, DM Friedmann, PP
Citation: Dm. Guillot et Pp. Friedmann, Fundamental aeroservoelastic study combining unsteady computational fluid mechanics with adaptive control, J GUID CON, 23(6), 2000, pp. 1117-1126
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