Journal of guidance, control and dynamics

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  Año 2001, Vol. 24, Número 6

  • Singular Perturbations and Time Scales in Guidance and Control of Aerospace Systems: A Survey

    D. S. Naidu, A. J. Calise

    págs. 1057-1078

    

  • Multi-Input/Multi-Output Reconfigurable Flight Control Design

    W. Siwakosit

    págs. 1079-1088

    

  • Input/Output Conditioning of Robust Integrated Flight and Propulsion Controller

    I. Postlethwaite, D. G. Bates, M. C. Turner

    págs. 1089-1099

    

  • Fuel-Optimal, Low-Thrust, Three-Dimensional Earth-Mars Trajectories

    S. R. Vadali, R. S. Nah

    págs. 1100-1107

    

  • Influence of a Small End Mass on Tether-Mediated Orbital Injection

    M. Ruiz, J. Pelaez

    págs. 1108-1117

    

  • Fast Algorithm for Prediction of Satellite Imaging and Communication Opportunities

    Y. Mai, P. Palmer

    págs. 1118-1124

    

  • Flight Mechanics of an Elastic Symmetric Missile

    W. H. Mermagen, C. H. Murphy

    págs. 1125-1132

    

  • Low Operational Order Analytic Sensitivity Analysis for Tree-Type Multibody Dynamic Systems

    Y. Hsu, K. S. Anderson

    págs. 1133-1143

    

  • Efficient Dynamical Equations for Gyrostats

    P. C. Mitiguy, K. J. Reckdahl

    págs. 1144-1156

    

  • Nonlinear Flight Control Using Forebody Tangential Blowing

    Y. Takahara, S. M. Rock

    págs. 1157-1166

    

  • Capture Set Computation of an Optimally Guided Missile

    T. Raivio

    págs. 1167-1175

    

  • Using a Multiple-Model Adaptive Estimator in a Random Evasion Missile/Aircraft Encounter

    J. Shinar, S. A. Weizman, Y. Oshman

    págs. 1176-1186

    

  • Kalman Filtering for Spacecraft System Alignment Calibration

    M. E. Pittelkau

    págs. 1187-1195

    

  • Literal Approximations to Aircraft Dynamic Modes

    N. Ananthkrishnan

    págs. 1196-1203

    

  • New Tools for Computing Tight Bounds on the Real Structured Singular Value

    I. Postlethwaite, D. G. Bates, M. J. Hayes

    págs. 1204-1213

    

  • Quaternion-Based Adaptive Attitude Tracking Controller Without Velocity Measurements

    B. T. Costic, M. S. de Queiroz, D. M. Dawson

    págs. 1214-1222

    

  • Adaptive Shunting for Vibration Control of Frequency-Varying Structures

    K.-H. Rew

    págs. 1223-1224

    

  • Level Flight Trim and Stability Analysis Using Extended Bifurcation and Continuation Procedure

    N. Ananthkrishnan

    págs. 1225-1227

    

  • Near-Eigenaxis Rotation Control Law Design for Moving-to-Rest Maneuver

    H.-S. Oh, Y.-K. Chang, J.-H. Hwang, Y.-D. Yoon

    págs. 1228-1230

    

  • Control Laws for Minimum Orbital Change-The Satellite Retrieval Problem

    D. B. Spencer, T. Cichan, R. G. Melton

    págs. 1231-1233