Journal of guidance, control and dynamics

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  Año 2000, Vol. 23, Número 3

  • Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying

    M. S. de Queiroz

    págs. 385-390

    

  • Federated Kalman Filtering Via Formation of Relation Equations in Augmented State Space

    V. A. Tupysev

    págs. 391-398

    

  • Receding Horizon Control Lyapunov Function Approach to Suboptimal Regulation of Nonlinear Systems

    J. Cloutier, M. Sznaier

    págs. 399-405

    

  • Closed-Loop System Identification by Residual Whitening

    C. H. Kuo, M. P. Schoen, S. Chinvorarat

    págs. 406-411

    

  • Accommodating a Class of Actuator Failures in Flight Control Systems

    R. A. Hess, W. Siwakosit

    págs. 412-419

    

  • Perspective Predictor/Flight-Path Display with Minimum Pilot Compensation

    G. Sachs

    págs. 420-429

    

  • Robust Variable Structure Controller Design for Fault Tolerant Flight Control

    Y. Kim, D. Kim

    págs. 430-437

    

  • Simulator Platform Motion Effects on Pilot-Induced Oscillation Prediction

    J. A. Schroeder

    págs. 438-444

    

  • Probabilistic Approach to Aircraft Performance Enhancement in Atmospheric Turbulence

    A. Pieracci, G. Mengali

    págs. 445-449

    

  • Gain-Scheduled Lateral Control of the F-14 Aircraft During Powered Approach Landing

    I. Fialho, G. J. Balas, A. K. Packard

    págs. 450-458

    

  • Adaptive Hysteresis Model for Model Reference Control with Actuator Hysteresis

    A. Kurdila, G. Webb, D. Lagoudas

    págs. 459-465

    

  • Evaluation of the Dynamic Environment of an Asterold: Applications to 433 Eros

    Daniel J. Scheeres, B. G. Williams

    págs. 466-475

    

  • Fuel-Optimal Planar Earth-Mars Trajectories Using Low-Thrust Exhaust-Modulated Propulsion

    S. R. Vadali

    págs. 476-482

    

  • Rapid Energy Dissipation in a Yo-Yo-Type Wire Boom Deployment System

    P. M. Kintner, M. L. Psiaki

    págs. 483-490

    

  • Optimal Vibration Control of Thin-Walled Anisotropic Cantilevers Exposed to Blast Loadings

    S. Na, L. Librescu

    págs. 491-500

    

  • Dynamics of a Variable-Mass, Flexible-Body System

    A. K. Banerjee

    págs. 501-508

    

  • Optimal Size and Location of Piezoelectric Actuator/Sensors: Practical Considerations

    O. J. Aldraihem

    págs. 509-515

    

  • Loop Shaping Design for Missile Autopilots: Controller Configurations and Weighting Filter Selection

    P. A. Iglesias

    págs. 516-525

    

  • Fast-Time Study of Airline-Influenced Arrival Sequencing and Scheduling

    H. Erzberger, G. C. Carr

    págs. 526-531

    

  • Accuracy of the Global Positioning System-Derived Acceleration Vector

    M. L. Psiaki, P. M. Kintner, S. P. Powell

    págs. 532-538

    

  • Predictive Missile Guidance

    J. P. Norton, R. A. Best

    págs. 539-546

    

  • Neural Networks and Adaptive Nonlinear Control of Agile Antlair Missiles

    M. B. McFarland

    págs. 547-553

    

  • Reduction of Propagated Satellite Yaw Errors Using Orbital Rate Coupling

    D. Bruno

    págs. 554-555

    

  • Strategy for Deployment of Multiple Satellites for Collision-Free Relative Orbital Motion

    R. V. Ramanan

    págs. 556-557

    

  • Minimization of Vibration of Spacecraft Appendages During Shape Control Using Smart Structures

    S. Kalaycioglu

    págs. 558-560

    

  • Spacecraft Formation Flying: Dynamics and Control

    J. M. Buffington, V. Kapila, A. G. Sparks

    págs. 561-563

    

  • Optimal Variable-Structure Control Tracking of Spacecraft Maneuvers

    J. L. Crassidis

    págs. 564-565

    

  • Parameters Selection for Baumgarte's Constraint Stabilization Method Using the Predictor-Corrector Approach

    J. N. Huang, S. T. Lin

    págs. 566-569

    

  • Application of a Dichotomic Basis Method to Performance Optimization of Supersonic Aircraft

    A. V. Rao

    págs. 570-572

    

  • Fuzzy-Logic-Based Closed-Loop Optimal Law for Homing Missiles Guidance

    N. Rahbar, M. B. Menhaj

    págs. 573-574