págs. 193-199
Laboratory Test System for Performance Evaluation of Advanced Star Sensors
G. Rufino, A. Moccia
págs. 200-208
Control of Chaotic Motion in a Dual-Spin Spacecraft with Nutational Damping
P. A. Meehan, S. F. Asokanthan
págs. 209-214
págs. 215-221
Characteristics of Time-Optimal Commands for Flexible Structures with Limited Fuel Usage
M. A. Lau, L. Y. Pao
págs. 222-231
Experiments on Command Shaping Control of a Manipulator with Flexible Links
Franco Bernelli-Zazzera, M. Romano, B. N. Agrawal
págs. 232-239
Galibration of Measurement Delay in Global Positioning System/Strapdown Inertial Navigation System
G.-I. Jee, H. K. Lee, J. G. Lee
págs. 240-247
Guidance Law Design by Adaptive Fuzzy Sliding-Mode Control
C.-F. Hsu, C.-M. Lin
págs. 248-256
Reduced-Order Entry Trajectory Planning for Acceleration Guidance
K. D. Mease, D. T. Chen
págs. 257-266
Robust Control System Design Using Simulated Annealing
T. Motoda, R. F. Stengel
págs. 267-274
págs. 275-284
Motion Control of a Nonholonomic System Based on the Lyapunov Control Method
T. Urakubo, K. Tsuchiya, K. Tsujita
págs. 285-290
Robust Fault Detection for Uncertain Discrete-Time Systems
J. Lam, H. Wang
págs. 291-301
Output Feedback Control of the Nonlinear Aeroelastic Response of a Slender Wing
M. J. Patil, D. H. Hodges
págs. 302-308
System Architecture Trades Using Bode-Step Control Design
F. Y. Hadaegh, A. Ghavimi, B. J. Lurie
págs. 309-315
Order Reduction and Closed-Loop Vibration Control in Helicopter Fuselages
A. Mathews, C. Venkatesan, V. R. Sule
págs. 316-323
Analysis of the Two-Degree-of-Freedom Wing Rock in Advanced Aircraft
R. V. Ramnath, T. H. Go
págs. 324-333
págs. 334-339
págs. 340-351
págs. 352-357
Turning Elliptic Orbital Planes via Intermediate Thrust Spherical Arcs
R. H. Bishop, D. M. Azimov
págs. 358-367
págs. 368-375
Nonlinear Tracking Control for Satellite Formations
A. Sparks, E. Nelson, H.-H. Yeh
págs. 376-386
Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft
H. Schaub, K. T. Alfriend
págs. 387-393
Event Detection and Characterization During Autonomous Interplanetary Navigation
T. P. Crain, R. H. Bishop
págs. 394-403
Adaptive Critic-Based Neural Networks for Agile Missile Control
D. Han, S. N. Balakrishnan
págs. 404-406
Jump Markovian-Based Control of Wing Deployment for an Uncrewed Air Vehicle
A. Stoica, I. Yaesh
págs. 407-410
págs. 411-414
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