págs. 417-418
Structural Damage Detection Using Virtual Passive Controllers
J.-N. Juang, J.-S. Lew
págs. 419-424
Time-Varying Linear Pursuit-Evasion Game Models with Bounded Controls
T. Shima, J. Shinar
págs. 425-432
Incremental-Angle and Angular Velocity Estimation Using a Star Sensor
T. K. Alex, G. N. Rao, M. S. Bhat
págs. 433-441
Classical/Neural Synthesis of Nonlinear Control Systems
S. Ferrari, R. F. Stengel
págs. 442-448
Rocket Nozzle Flow Control Using a Reduced-Order Computational Fluid Dynamics Model
D. J. Lucia, P. S. Beran, M. Pachter
págs. 449-454
págs. 455-463
págs. 464-473
págs. 474-481
págs. 482-493
Predictor/Flight-Path Display for Manual Longitudinal Control Improvement
K. Dobler, G. Sachs
págs. 494-501
págs. 502-509
págs. 510-516
M. Pachter, N. J. Schindeler
págs. 517-527
Online Parameter Estimation Techniques Comparison Within a Fault Tolerant Flight Control System
G. Campa, M. Napolitano, Y. Song
págs. 528-537
Semi-Analytical Formulas for Launcher Performance Evaluation
P. Teofilatto, E. Di Sotto
págs. 538-545
Identification of the Dominant Ground Handling Characteristics of a Navy Jet Trainer
R. E. Magdaleno, J. G. Reinsberg, D. H. Klyde, T. T. Myers
págs. 546-552
Guidance and Relative Navigation for Autonomous Rendezvous in a Circular Orbit
H. B. Hablani, M. L. Tapper, D. J. Dana-Bashian
págs. 553-562
Anatomy of the Constant Radial Thrust Problem
M. R. Akella, R. A. Broucke
págs. 563-570
págs. 571-581
Tests of Magnetometer/Sun-Sensor Orbit Determination Using Flight Data
M. L. Psiaki, H. Jung
págs. 582-590
Minimizing the Effects of Transverse Torques During Thrusting for Spin-Stabilized Spacecraft
J. A. Oldenburg, S. G. Tragesser
págs. 591-595
Increasing the Numerical Robustness of Balanced Model Reduction
G. J. W. Mallory
págs. 596-598
Spillover Suppression via Eigenstructure Assignment in Large Flexible Structures
U. S. Park, J. W. Choi
págs. 599-601
Solar Sail Hybrid Trajectory Optimization for Non-Keplerian Orbit Transfers
C. R. McInnes, G. W. Hughes
págs. 602-603
págs. 604-606
págs. 607-608




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