Journal of guidance, control and dynamics

• 

  Año 2005, Vol. 28, Número 4

  • History of Low-Order Equivalent Systems for Aircraft Flying Qualities

    J. Hodgkinson

    págs. 577-583

    

  • Magnetometer-Based Attitude and Rate Estimation for Spacecraft with Wire Booms

    T. E. Humphreys

    págs. 584-593

    

  • Estimation of a Spacecraft's Attitude Dynamics Parameters by Using Flight Data

    M. L. Psiaki

    págs. 594-603

    

  • Estimation of Postlaunch Angular Motion for Kinetic Energy Projectiles

    W. C. Pickel

    págs. 604-610

    

  • Dynamic Stability of Electrodynamic Tethers in Inclined Elliptical Orbits

    Y. N. Andres, J. Pelaez

    págs. 611-622

    

  • Free-Flying Robot Tested on Parabolic Flights: Kinematic Control

    C. Menon, A. Bulgarelli, S. Cocuzza, A. Aboudan

    págs. 623-630

    

  • Classical and Simple Adaptive Control for Nonminimum Phase Autopilot Design

    I. Barkana

    págs. 631-638

    

  • Robustness Analysis of Nonlinear Flight Controllers

    C. Papageorgiou

    págs. 639-648

    

  • Reliability-Based Control Design for Uncertain Systems

    S. P. Kenny, L. G. Crespo

    págs. 649-658

    

  • Velocity-Free Attitude Controllers Subject to Actuator Magnitude and Rate Saturations

    M. R. Akella, A. Valdivia, G. R. Kotamraju

    págs. 659-666

    

  • Nonlinear Control for Reconfiguration of Unmanned-Aerial-Vehicle Formation

    S. Venkataramanan, A. Dogan

    págs. 667-678

    

  • Robust Analysis for Missile Lateral Acceleration Control Using Finite Inclusion Theorem

    A. Tsourdos, B. A. White, L. Bruyere

    págs. 679-685

    

  • Hybrid Optimal Control Framework for Mission Planning

    C. N. D Souza, I. M. Ross

    págs. 686-697

    

  • Flight Testing of a Reconfigurable Control System on an Unmanned Aircraft

    D. Shore, M. Bodson

    págs. 698-707

    

  • Line-of-Sight Guidance Laws for Formation Flight

    M.-J. Tahk, C.-S. Park, C.-K. Ryoo

    págs. 708-716

    

  • Improved Integer Ambiguity Resolution Technique for Fixed Arrays

    J. D. Wolfe, J. L. Speyer

    págs. 717-723

    

  • Optimal Guidance Laws with Terminal Impact Angle Constraint

    C.-K. Ryoo

    págs. 724-732

    

  • Derivation of Formation-Flight Guidance Laws for Unmanned Air Vehicles

    J. Z. Ben-Asher, S. Segal

    págs. 733-742

    

  • Calibration and Attitude Determination with Redundant Inertial Measurement Units

    M. E. Pittelkau

    págs. 743-752

    

  • Analytical Gradients for Gravity Assist Trajectories Using Constant Specific Impulse Engines

    C. A. Ocampo, S. Zimmer

    págs. 753-760

    

  • Relative Motion Between Elliptic Orbits: Generalized Boundedness Conditions and Optimal Formationkeeping

    P. Gurfil

    págs. 761-767

    

  • Proposed Method for Modeling the Gravitational Interaction Between Finite Bodies

    J. Ashenberg

    págs. 768-774

    

  • Optimizing Finite-Burn, Round-Trip Trajectories with I~s~p Constraints and Mass Discontinuities

    C. A. Ocampo, C. L. Ranieri

    págs. 775-781

    

  • Design of Spacecraft Formation Orbits Relative to a Stabilized Trajectory

    F. Y. Hsiao, Daniel J. Scheeres

    págs. 782-794

    

  • Fuel-Optimal Transfers Between Coplanar Circular Orbits Using Variable-Specific-Impulse Engines

    C. M. Roithmayr, H. Seywald

    págs. 795-800

    

  • Fast Graph-Search Algorithms for General-Aviation Flight Trajectory Generation

    E. Rippel, A. Bar-Gill

    págs. 801-811

    

  • Second-Order Necessary Conditions and Sufficient Conditions Applied to Continuous-Thrust Trajectories

    J. E. Prussing, S. L. Sandrik

    págs. 812-815

    

  • Model Predictive Control of a Parafoil and Payload System

    N. Slegers, M. Costello

    págs. 816-820

    

  • Terminal Guidance Law Based on Proportional Navigation

    Y. Ulybyshev

    págs. 821-823

    

  • Cross-Track Motion of Satellite Formations in the Presence of J~2 Disturbances

    S. A. Schweighart

    págs. 824-825