Identification and Retuning of Optimum Delayed Feedback Vibration Absorber
N. Jalili, N. Olgac
págs. 961-970
Safety Constrained Free-Flyer Path Planning at the International Space Station
A. B. Roger, C. R. McInnes
págs. 971-979
Online Estimation of Allan Variance Parameters
J. J. Ford, M. E. Evans
págs. 980-987
Gain-Scheduled Control: Relaxing Slow Variation Requirements by Velocity-Based Design
W. E. Leithead, D. J. Leith
págs. 988-1000
Robust H~¿ Deconvolution and Its Application to Fault Detection
U. Shaked, I. Yaesh
págs. 1001-1012
págs. 1013-1020
págs. 1021-1029
págs. 1030-1036
Decentralized Design for Integrated Flight/Propulsion Control of Aircraft
Z. Chen, P. G. Voulgaris
págs. 1037-1044
Quantitative Cross-Feed and Feedback Design of Helicopter in near Hover Flight
U. I. Ukpai, O. D. I. Nwokah
págs. 1045-1054
R. E. Skelton, C. Sultan, M. Corless
págs. 1055-1064
Analytic Steady-State Accuracy of a Spacecraft Attitude Estimator
F. L. Markley, R. G. Reynolds
págs. 1065-1066
Robust H~2 Estimation with Application to Robust Fault Detection
E. G. Collins, T. Song
págs. 1067-1071
págs. 1072-1075
págs. 1076-1077
Collision Dynamics for Space Tethers
P. Trivailo, C. Blanksby
págs. 1078-1080
Two Projectiles Connected by a Flexible Tether Dropped in the Atmosphere
G. Frost, M. Costello
págs. 1081-1084
New Method for Extracting the Quaternion from a Rotation Matrix
I. Y. Bar-Itzhack
págs. 1085-1087
págs. 1088-1089
Review of Spectral Methods in MATLAB
F. Fahroo
págs. 1091-1092
Benchmark Active Control Technology Special Section: Part II
V. Mukhopadhyay
pág. 1093
Comparison of Two Navier-Stokes Methods with Benchmark Active Control Technology Experiments
D. M. Schuster, R. E. Bartels
págs. 1094-1099
Active Control of Wind-Tunnel Model Aeroelastic Response Using Neural Networks
R. C. Scott, L. E. Pado
págs. 1100-1108
Adaptive Output Feedback Control of a Nonlinear Aeroelastic Structure
S. N. Singh, W. Xing
págs. 1109-1116
P. P. Friedmann, D. M. Guillot
págs. 1117-1126
págs. 1127-1133
págs. 1134-1139
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