Journal of guidance, control and dynamics

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  Año 2005, Vol. 28, Número 2

  • Editorial: Battin Birthday Issue

    G. T. Schmidt

    pág. 193

    

  • Global Search for Idealized Free-Return Earth-Mars Cyclers

    R. P. Russell, C. A. Ocampo

    págs. 194-208

    

  • Optimization of Biimpulsive Trajectories in the Earth-Moon Restricted Three-Body System

    A. A. Quarta, G. Mengali

    págs. 209-216

    

  • Nonimpact Lunar Transfer Trajectories Using the Pseudostate Technique

    V. Adimurthy, R. V. Ramanan

    págs. 217-225

    

  • Real-Time Navigation of Formation-Flying Spacecraft Using Global-Positioning-System Measurements

    O. Montenbruck, S. Leung

    págs. 226-235

    

  • Adjoint Method for Missile Performance Analysis on State-Space Models

    M. Weiss

    págs. 236-248

    

  • Simple Strategy for Geostationary Stationkeeping Maneuvers Using Solar Sail

    C. Circi

    págs. 249-253

    

  • Evaluation and Comparison of Relative Motion Theories

    K. T. Alfriend

    págs. 254-261

    

  • Formation Establishment and Reconfiguration Using Impulsive Control

    K. T. Alfriend, S. S. Vaddi

    págs. 262-268

    

  • Libration Control of Electrodynamic Tethers in Inclined Orbit

    Enrico C. Lorenzini, J. Pelaez

    págs. 269-279

    

  • Low-Thrust Variable-Specific-Impulse Transfers and Guidance to Unstable Periodic Orbits

    A. Capella, J. Senent, C. A. Ocampo

    págs. 280-290

    

  • Dynamic Behavior of an Orbiter Around Europa

    Martín Lara Coira, Juan Félix San Juan Díaz

    págs. 291-297

    

  • Effects of Orbital Parameter Uncertainties

    D. Izzo

    págs. 298-305

    

  • Optimization of Roundtrip, Time-Constrained, Finite Burn Trajectories via an Indirect Method

    C. A. Ocampo, C. L. Ranieri

    págs. 306-314

    

  • Realistic Earth Escape Strategies for Solar Sailing

    M. Macdonald, C. R. McInnes

    págs. 315-323

    

  • Use of Analytical Gradients to Calculate Optimal Gravity-Assist Trajectories

    S. Zimmer, C. A. Ocampo

    págs. 324-332

    

  • Low-Thrust Guidance Scheme for Earth-Capture Trajectories

    C. A. Kluever, Y. Gao

    págs. 333-342

    

  • Control of Hovering Spacecraft Near Small Bodies: Application to Asteroid 25143 Itokawa

    Daniel J. Scheeres, S. B. Broschart

    págs. 343-354

    

  • Time- and Phase-Space Stability Analysis of the Jupiter-Sun System

    D. G. Tuckness

    págs. 355-359

    

  • Steady-State Matched Model Reduction for Flexible Structures with Accelerometer Measurements

    T. Williams

    págs. 360-362

    

  • Convergence of Newton's Method via Lyapunov Analysis

    R. D. Robinett, Jorge Eduardo Hurtado Gómez

    págs. 363-364

    

  • Spacecraft Planetary Capture Using Gravity-Assist Maneuvers

    M. Macdonald, C. R. McInnes

    págs. 365-368

    

  • Optimal Orbital Transfer with Electrodynamic Tether

    P. Williams

    págs. 369-371

    

  • Lunar Base for Mars Missions

    C. Circi

    págs. 372-373

    

  • Earth Escape Using a Slowly Rotating, Doubly Reflective Solar Sail

    M. A. Swartwout

    págs. 374-376

    

  • Vibration Suppression of Flexible Spacecraft During Attitude Maneuvers

    G. Ma, Q. Hu

    págs. 377-379

    

  • Dynamics of a Particle Moving Along an Orbital Tower

    C. R. McInnes

    págs. 380-382