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    Output-based disturbance rejection control for nonlinear uncertain systems with unknown frequency disturbances using an observer backstepping approach

    Freier Zugriff
    Yang, Jun / Ding, Zhengtao / Chen, Wen-Hua et al. | BASE | 2016
    Schlagwörter: Output feedback control; Nonlinear uncertain system; Multiple disturbances and uncertainties; Internal model principle; Missile roll stabilization

    Aerodynamic Characteristics of 0.187-Scale Model of a Target Missile at Mach 1.80 to 2.16

    W. A. Corlett | NTIS | 1966
    Schlagwörter: Missile roll control , Stability and control , Control , Missile , Roll

    Alternative Polar Homing Strategies

    M. S. Gate / R. S. Randall | NTIS | 1989
    Schlagwörter: Missile Guidance & Control Systems , Missile control , Missile design , Roll

    The Effectiveness of Different Methods of Reducing the Dispersion of Experimental Missiles (Efficacite de Differents Procedes pour Reduire la Dispersion des Missiles Experimentaux)

    M. Bismut | NTIS | 1964
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Guided missile trajectories , Flight control systems , Control systems , Attitude control systems , Roll , Control jets , Control , Missile dispersion

    Optimal nonlinear tracking control for BTT missiles using polynomial feedback

    Song-Kuo Chang / King Yuan | Tema Archiv | 1990
    Schlagwörter: AEROSPACE CONTROL , ATTITUDE CONTROL , BANK TO TURN CONTROL , MISSILE PERFORMANCE , BANK-TO-TURN MISSILE , ROLL , OPTIMAL NONLINEAR TRACKING CONTROL , NONLINEAR MISSILE MODEL

    Approximate Optimum Control of the Angle of Roll in the Problem of the Re-Entry of Hypersonic Vehicles

    V. T. Pashintsev | NTIS | 1975
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Roll , Control theory

    Static Aerodynamic Stability Characteristics of Bodies of Revolution with Wraparound Fins at Mach Numbers from 1.6 to 2.86

    J. E. Vaughn / C. W. Dahlke / J. C. Craft | NTIS | 1972
    Schlagwörter: Missile Guidance & Control Systems , Roll

    Tertiary Injector for Propulsion System Roll Control

    B. A. Jones | NTIS | 1966
    Schlagwörter: Missile Technology , Control systems , Roll , Thrust vector control systems

    Role of Separation Autopilots for Modern Missile Concepts

    R. Deslandes | NTIS | 1990
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Missile Guidance & Control Systems , Missile tests , Roll , Missile guidance

    New Guidance Law to Improve the Accuracy of Tactical Missiles

    W. R. Chadwick | NTIS | 1983
    Schlagwörter: Missile Guidance & Control Systems , Guided missile components , Guided missile trajectories , Aerodynamic control surfaces , Roll free gyroscopes

    Optical Attitude Reference

    W. E. Miller / R. L. Sitton / A. D. Blackmon | NTIS | 1976
    Schlagwörter: Missile Guidance & Control Systems , Guided missile components , Roll

    Factory Acceptance Testing of Missile 26E

    NTIS | 1961
    Schlagwörter: Missile Technology , Flight control systems , Roll , Propellant control , Guided missile safety

    Review and Comparison of Tactical Missile Control Methods

    R. H. Nunn | NTIS | 1972
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Guided missile trajectories , Attitude control systems , Aerodynamic control surfaces , Guided missile components , Roll , Thrust vector control systems , Boundary layer control , Control jets , Jet interaction control systems

    The Influence of Structural Elasticity on the Stability of Airplanes and Multi-Stages Missiles

    L. T. Prince | NTIS | 1961
    Schlagwörter: Missile Technology , Flight control systems , Altitude control systems , Roll , Adaptive control systems

    Simulation of the Flight of a Short Range Air Defense System Rocket Before Radar Acquisition

    J. E. Cochran / J. R. Beaty | NTIS | 1977
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Guided missile trajectories , Control , Roll , Guided missile launchers

    Design of Control Surfaces

    Sadraey, Mohammad H. | Wiley | 2012
    Schlagwörter: control surface selection, function of aircraft configuration , fighter aircraft/missile maneuverability, branch of controllability , configuration selection of control surfaces , control systems, redundancy in achieving two orders of magnitude , design of control surfaces , dutch‐roll problems, yaw damper changing lateral‐directional stability , control, flight condition from trim to final or new trim point , lateral‐directional hitting aircraft, in rolling, spiral/dutch‐roll oscillation

    Aerodynamic Methodology. Bodies with Tails at Arbitrary Roll Angle

    J. E. Fidler / M. C. Bateman | NTIS | 1974
    Schlagwörter: Missile Guidance & Control Systems , Roll

    Analysis of the MISTIC System Autopilots

    R. E. Alongi / M. D. Rezmer | NTIS | 1970
    Schlagwörter: Navigation, Guidance, & Control , Flight control systems , Roll , Mistic(Missile system target illuminator controlled) , Missile system target illuminator controlled

    A S-204/Lm-1 L/V Operational Alternate Mission Trajectories

    A. Genter | NTIS | 1967
    Schlagwörter: Control stability , Trajectory control , Missile trajectories , Roll

    Aerodynamic and Flight Simulation Study II. Volume I

    C. A. Lindle | NTIS | 1969
    Schlagwörter: Missile Technology , Roll , Aerodynamic control surfaces

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