Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros
C. Heiberg, B. Wie, D. Bailey
págs. 865-872
págs. 873-878
págs. 879-886
Limit Cycle Oscillation Prediction Using Artificial Neural Networks
M. R. Johnson, C. M. Denegri
págs. 887-895
págs. 896-902
págs. 903-909
Adaptive Neurocontroller for a Nonlinear Combat Aircraft Model
M. Battipede, P. A. Gili
págs. 910-917
Design of an Aeroelastic Delta Wing Model for Active Flutter Control
R. E. Richard, J. A. Rule
págs. 918-924
Precision of Satellite Laser Ranging Calibration of the Naval Space Surveillance System
G. C. Gilbreath, P. W. Schumacher
págs. 925-932
págs. 933-938
Nonlinear Regulation for Tracking and Drag Compensation of Two-Body Spinning Satellite
P. Di Giamberardino
págs. 939-952
Bifurcation Analysis of Attitude Dynamics in Rigid Spacecraft with Switching Control Logics
G. de Matteis, G. Avanzini
págs. 953-959
págs. 960-966
mu Synthesis for a Large Flexible Space Structure Experimental Testbed
B. Boulet, B. A. Francis
págs. 967-977
P. M. Bainum, I. M. Fonseca
págs. 978-982
Iterative Algorithms for Attitude Estimation Using Global Positioning System Phase Measurements
A. Nadler, I. Y. Bar-Itzhack
págs. 983-990
págs. 991-997
Applications of Global Positioning System Velocity-Based Attitude Information
R. P. Kornfeld, R. J. Hansman
págs. 998-1008
Practical Dual-Control Guidance Using Adaptive Intermittent Maneuver Strategy
H.-I. Lee, M.-J. Tahk
págs. 1009-1015
Partial Aircraft State Estimation from Visual Motion Using the Subspace Constraints Approach
P. Gurfil, H. Rotstein
págs. 1016-1028
págs. 1029-1031
págs. 1032-1034
págs. 1035-1036
Rate Feedback Control of Free-Free Uniform Flexible Rod
Y. Halevi, N. Raskin
págs. 1037-1039
Reducing Minimum Time for Flexible Body Small-Angle Slewing with Vibration Suppression
A. K. Banerjee
págs. 1040-1042
Optimal Control Bolza and Transformed Mayer Problems with Feedback Linearized State Equations
J. Franch, S. K. Agrawal
págs. 1043-1045
págs. 1046-1048
Uniform Damping of Plates Using a Modified Nodal Control Method
G. Washington, J.-K. Song
págs. 1049-1052
H~¿ Feedback for Attitude Control of Liquid-Filled Spacecraft
A. Y. T. Leung, J. Kuang
pág. 1053
F. Fahroo
págs. 1054-1055
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