Journal of guidance, control and dynamics

• 

  Año 2001, Vol. 24, Número 4

  • Tuning of Coning Algorithms to Gyro Data Frequency Response Characteristics

    J. G. Mark, D. A. Tazartes

    págs. 641-647

    

  • Eigenstructure vs Constrained H^¿ Design for Hypersonic Winged Cone

    P. Lohsoonthorn

    págs. 648-658

    

  • Design of Missile Guidance Law via Variable Structure Control

    J. Moon, K. Kim, Y. Kim

    págs. 659-664

    

  • Stable Neuro-Flight-Controller Using Fully Tuned Radial Basis Function Neural Networks

    Y. Li, N. Sundararajan, P. Saratchandran

    págs. 665-674

    

  • Nonlinear Adaptive Flight Control Using Backstepping and Neural Networks Controller

    T. Lee, Y. Kim

    págs. 675-682

    

  • Adaptive Fuzzy Gain Scheduling in Guidance System Design

    H.-W. Su, C.-L. Lin

    págs. 683-692

    

  • Comparison of Intelligent, Adaptive, and Nonlinear Flight Control Laws

    M. L. Steinberg

    págs. 693-699

    

  • Fixed-Range Optimal Trajectories of Supersonic Aircraft by First-Order Expansions

    R. Windhorst

    págs. 700-709

    

  • Neighboring Optimal Aircraft Guidance in Winds

    M. R. Jardin, A. E. Bryson

    págs. 710-715

    

  • General Method for Calculating Satellite Collision Probability

    R. P. Patera

    págs. 716-722

    

  • Constant Tangential Low-Thrust Trajectories near an Oblate Planet

    A. A. Sukhanov, A. F. B. De APrado

    págs. 723-731

    

  • Thrust Limited Coplanar Aeroassisted Orbital Transfer

    H. Baumann

    págs. 732-738

    

  • Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations

    H. Schaub, K. T. Alfriend

    págs. 739-745

    

  • Approximate Solutions for Tethered Satellite Motion

    J. E. Cochran, T. A. Lovell, S. Cho

    págs. 746-754

    

  • Adaptive Attitude Control of Spacecraft: Mixed H~2/H~¿ Approach

    C.-S. Wu, B.-S. Chen

    págs. 755-766

    

  • Optimal Stabilization of Takagi-Sugeno Fuzzy Systems with Application to Spacecraft Control

    M.-J. Tahk, Y. Park

    págs. 767-777

    

  • Stability Analysis of Planetary Satellite Orbiters: Application to the Europa Orbiter

    Daniel J. Scheeres

    págs. 778-787

    

  • Optimal Reorientation of a Multibody Spacecraft Through Joint Motion Using Averaging Theory

    W. T. Cerven, V. L. Coverstone

    págs. 788-795

    

  • Computational Aspects of Transfer Trajectories to Halo Orbits

    J. A. Kechichian

    págs. 796-804

    

  • New Modeling and Control Design Techniques for Smart Deformable Aircraft Structures

    R. K. Yedavalli, S.-K. Kwak

    págs. 805-815

    

  • Robust Minimum Power/Jerk Control of Maneuvering Structures

    T. A. Hindle

    págs. 816-826

    

  • Tethered Robot Casting Using a Spacecraft-Mounted Manipulator

    D. N. Nenchev, M. Nohmi

    págs. 827-833

    

  • Experimental Evaluation of Flexible Manipulator Trajectory Optimization

    I. Sharf, B. Pond

    págs. 834-843

    

  • Selective Modal Control Theory for Piezolaminated Anisotropic Shells

    S. E. Miller

    págs. 844-852

    

  • Generalization of D'Alembert's Method for Applications to Dynamics

    R. X. Meyer

    págs. 853-854

    

  • Closed-Loop Control Tests for Vertical Fin Buffeting Alleviation Using Strain Actuation

    F. Nitzsche, D. G. Zimcik

    págs. 855-856

    

  • Digital Redesign of Linear State-Feedback Law via Principle of Equivalent Areas

    T. Ieko, K. Kanai, Y. Ochi

    págs. 857-858

    

  • Variable Structure Controller Design with Application to Missile Tracking

    M. S. Bhat, K. N. Swamy, A. A. Powly, D. S. Bai

    págs. 859-862

    

  • Review of Fundamentals of Kalman Filtering: A Practical Approach. Progress in Astronautics and Aeronautics, Vol. 190

    J. R. Cloutier

    págs. 863-864