Journal of guidance, control and dynamics

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  Año 2006, Vol. 29, Número 6

  • Genesis of Three-Axis Spacecraft Guidance, Control, and On-Orbit Stabilization

    J. C. Herther, J. S. Coolbaugh

    págs. 1247-1270

    

  • Tailored Dynamic Gain-Scheduled Control

    M. H. Lowenberg, Chris D.C. Jones, T. S. Richardson

    págs. 1271-1281

    

  • Quasilinear Parameter-Varying Autopilot Design Using Polynomial Eigenstructure Assignment with Actuator Constraints

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

    págs. 1282-1294

    

  • Spacecraft Line-of-Sight Control Using a Single Variable-Speed Control Moment Gyro

    P. Tsiotras, H. Yoon

    págs. 1295-1308

    

  • Linear Feedback Control Using Quasi Velocities

    A. J. Sinclair, Jorge Eduardo Hurtado Gómez, J. L. Junkins

    págs. 1309-1314

    

  • Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle

    C. E. Hall, Y. B. Shtessel

    págs. 1315-1328

    

  • Attitude Determination Using a Single-Star Sensor and a Star-Density Table

    J. Chun, J. Wang

    págs. 1329-1338

    

  • Simplified Technique for Modeling Piloted Rotorcraft Operations Near Ships

    R. A. Hess

    págs. 1339-1349

    

  • Affine Parameter-Dependent Preview Control for Rotorcraft Terrain Following Flight

    N. Paulino, C. Silvestre

    págs. 1350-1359

    

  • Indirect Optimization of Spiral Trajectories

    C. A. Ocampo, C. L. Ranieri

    págs. 1360-1366

    

  • Nonlinear Mapping of Gaussian Statistics: Theory and Applications to Spacecraft Trajectory Design

    Daniel J. Scheeres, R. S. Park

    págs. 1367-1375

    

  • On the Lyapunov Stability of Stationary Points Around a Central Body

    Teodoro López Moratalla, Antonio Elipe Sánchez

    págs. 1376-1383

    

  • Models for Rhumb-Line Attitude Maneuvers and Error Propagation Effects

    J. C. van der Ha

    págs. 1384-1394

    

  • Optimal Balanced-Energy Formation Flying Maneuvers

    F. Y. Hadaegh, A. Rahmani, M. Mesbahi

    págs. 1395-1403

    

  • Linear Covariance Techniques for Orbital Rendezvous Analysis and Autonomous Onboard Mission Planning

    D. K. Geller

    págs. 1404-1414

    

  • Performance Optimization for a Towed-Cable System with Attached Wind Sock

    P. Williams, P. Trivailo

    págs. 1415-1416

    

  • Simple Practical Classical-H~2 Optimal Robust Controller

    V. Radisavljevic-Gajic

    págs. 1417-1419

    

  • Solving Linear and Quadratic Quaternion Equations

    J. D. Turner

    págs. 1420-1422

    

  • Aeroservoelastic Stability of Supersonic Slender-Body Flight Vehicles

    H. Haddadpour

    págs. 1423-1426

    

  • Estimation of the Region of Attraction for State-Dependent Riccati Equation Controllers

    M. Innocenti, A. Bracci

    págs. 1427-1429

    

  • Equilibrium Configurations of a Four-Body Tethered System

    A. A. Correa

    págs. 1430-1434

    

  • Direct Trajectory Optimization and Costate Estimation via an Orthogonal Collocation Method

    T. P. Thorvaldsen, G. T. Huntington, D. A. Benson

    págs. 1435-1439

    

  • Ant Colony Algorithms for Two-Impulse Interplanetary Trajectory Optimization

    G. Radice

    págs. 1440-1443

    

  • Deadbeat Predictive Control on a Space Truss Structure

    L. Dozio

    págs. 1444-1445

    

  • Parametric Optimization Analysis for Minimum-Fuel Low-Thrust Coplanar Orbit Transfer

    D. Sheu, Y. Chen

    págs. 1446-1450

    

  • Equilibrium Control of Electrodynamic Tethered Satellite Systems in Inclined Orbits

    X. Zhou

    págs. 1451-1453

    

  • Probabilistic Robust Linear Parameter-Varying Control of an F-16 Aircraft

    F. Wu, B. Lu

    págs. 1454-1459

    

  • Guidance Law for an Air-Breathing Launch Vehicle Using Predictive Control Concept

    S. Dasgupta, V. Brinda

    págs. 1460-1463

    

  • Optimal Control Laws for Momentum-Wheel Desaturation Using Magnetorquers

    A. A. Quarta, F. Giulietti

    págs. 1464-1467

    

  • Collision Probability for Larger Bodies Having Nonlinear Relative Motion

    R. P. Patera

    págs. 1468-1471