Attitude Control System of the Wilkinson Microwave Anisotropy Probe
J. R. O Donnell, F. L. Markley, S. F. Andrews
págs. 385-397
Cybernetic Analysis of Perspective Flight-Path Display Dimensions
M. Mulder, J. A. Mulder
págs. 398-411
págs. 412-420
Path Planning and Open-Loop Shape Control of Modular Tensegrity Structures
R. E. Skelton, M. Masic
págs. 421-430
Fast In-Flight Detection of Flutter Onset: A Statistical Approach
A. Benveniste, M. Basseville, L. Mevel
págs. 431-438
Attitude and Orbit Control of a Very Large Geostationary Solar Power Satellite
B. Wie, C. M. Roithmayr
págs. 439-451
Suppression of Control Reversal Using Leading- and Trailing-Edge Control Surfaces
T. W. Strganac, G. Platanitis
págs. 452-460
Linear Parameter-Varying Detection Filter Design for a Boeing 747-100/200 Aircraft
I. Szaszi, G. J. Balas, A. Marcos
págs. 461-470
Interior-Point Algorithms for Control Allocation
J. A. M. Petersen
págs. 471-480
H Inverse Optimal Attitude-Tracking Control of Rigid Spacecraft
K.-V. Ling, W. Luo, Y.-C. Chu
págs. 481-493
Linear Parameter-Varying Antiwindup Compensation for Enhanced Flight Control Performance
F. Wu, S. Kim, B. Lu
págs. 494-505
págs. 506-515
Robust Neurocontrollers for Systems with Model Uncertainties: A Helicopter Application
Z. Huang, S. N. Balakrishnan
págs. 516-523
Adaptive Trajectory Control for Autonomous Helicopters
S. K. Kannan, E. N. Johnson
págs. 524-538
págs. 539-540
Equilibrium-to-Equilibrium Maneuvers of Rigid Electrodynamic Tethers
S. K. Agrawal, K. K. Mankala
págs. 541-545
pág. 546
Optimal Continuous Thrust Orbit Transfer Using Evolutionary Algorithms
J. Igarashi, D. B. Spencer
págs. 547-549
Control Law for Active Structural Damping Using a Control Moment Gyro
J.-F. Shi, C. J. Damaren
págs. 550-552
págs. 553-557
Nonlinear Control Allocation Using Piecewise Linear Functions: A Linear Programming Approach
M. A. Bolender
págs. 558-561
Stability Criteria of Slosh Motion with Periodicity in a Spinning Spacecraft
J. E. Cochran, J.-Y. Kang
págs. 562-567
Variable Structure Control of Unsteady Aeroelastic System with Partial State Information
S. N. Singh, S. Gujjula
págs. 568-573
C. A. Woolsey
págs. 574-575
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