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keywords:(Control

    A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model

    Lovell, Powell M , Jr / Stassi, Paul P | NTRS | 1950
    Keywords: LATERAL CONTROL DEVICES , STABILITY & CONTROL, LATERAL

    A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps

    Lovell, Powell M , Jr | NTRS | 1950
    Keywords: LATERAL CONTROL DEVICES , STABILITY & CONTROL, LATERAL

    Active heat rejection system on Mars Exploration Rover - design changes from Mars Pathfinder

    Patzold, J. D. / McGrath, P. L. / Tsuyuki, G. T. et al. | NTRS | 2003
    Keywords: control

    A design method for an optimal attitude regulator for a spinning space station

    Rempfer, P. S. | NTRS | 1967
    Keywords: OPTIMAL CONTROL , FEEDBACK CONTROL SYSTEM , ATTITUDE CONTROL

    Aerodynamic braking trajectories for mars orbit attainment.

    Finch, T. W. | NTRS | 1965
    Keywords: TRAJECTORY CONTROL

    Aerodynamic Characteristics and Flap Loads of Perforated Double Split Flaps on a Rectangular NACA 23012 Airfoil

    Turner, Thomas R | NTRS | 1943
    Keywords: WING FLAPS, DIVE-CONTROL

    Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel

    Liddell, Robert B | NTRS | 1942
    Keywords: WING FLAPS, DIVE-CONTROL

    AERODYNAMIC CHARACTERISTICS OF FOUR-DUCT TANDEM VTOL-AIRCRAFT CONFIGURATIONS

    Newsom, W. A., Jr. | NTRS | 1963
    Keywords: STABILITY AND CONTROL

    AERODYNAMIC CHARACTERISTICS OF TWO RECTANGULAR-PLAN-FORM, ALLMOVABLE CONTROLS IN COMBINATION WITH A SLENDER BODY OF REVOLUTION AT MACH NUMBERS FROM 3.00 TO 6.25

    Gloria, H. R. / Wong, T. J. | NTRS | 1955
    Keywords: CONTROL SURFACE

    Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7

    Turner, M J / Rabinowitz, S | NTRS | 1950
    Keywords: CONTROL SURFACES - HINGE MOMENTS , FLUTTER - CONTROL SURFACES

    AERODYNAMIC CONTROL OF DECELERATION AND RANGE FOR THE LUNAR MISSION

    Pritchard, E. B. | NTRS | 1962
    Keywords: CONTROL

    Aerodynamic damping and oscillatory stability in pitch for a model of a typical subsonic jet-transport airplane

    Brower, M. L. / Wright, B. R. | NTRS | 1966
    Keywords: PITCH CONTROL

    Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers from 0.6 to 18

    Gloria, H. R. / Sarabia, M. F. / Syvertson, C. A. | NTRS | 1958
    Keywords: STATIC STABILITY AND CONTROL

    AERODYNAMICS OF TRAJECTORY CONTROL FOR REENTRY AT ESCAPE SPEED

    Baradell, D. L. / Becker, J. V. / Pritchard, E. B. | NTRS | 1961
    Keywords: TRAJECTORY CONTROL

    Aeroelastic stability and control of an oblique wing

    Jones, R. T. / Nisbet, J. W. | NTRS | 1976
    Keywords: Aircraft Stability And Control

    Aeroelastic stability and control of an oblique wing - Wind tunnel experiments

    Jones, R. T. | NTRS | 1976
    Keywords: Aircraft Stability And Control

    AIRCRAFT VORTEX WAKES IN RELATION TO TERMINAL OPERATIONS

    Reeder, J. P. / Wetmore, J. W. | NTRS | 1963
    Keywords: AIR TRAFFIC CONTROL

    ALBURQUERQUE. RADAR BACK-SCATTER THEORIES FOR NEAR-VERTICAL INCIDENCE AND THEIR APPLICATION TO AN ESTIMATE OF THE LUNAR SURFACE ROUGHNESS

    Hayre, H. S. / Moore, R. K. | NTRS | 1962
    Keywords: RADAR APPROACH CONTROL /RAPCON/

    A look into strap-down guidance design. I.

    Otten, D. D. | NTRS | 1966
    Keywords: GIMBALLED CONTROL

    An analysis of a nonlinear instability in the implementation of a VTOL control system during hover

    Weber, J. M. | NTRS | 1982
    Keywords: Aircraft Stability And Control

    An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits

    Barker, L. K. / Sparrow, G. W. | NTRS | 1966
    Keywords: THRUST VECTOR CONTROL /TVC/

    An Autonomous Sensor-Based Path-Planner for Planetary Microrovers

    Burdick, J. / Laubach, S. | NTRS | 1998
    Keywords: control

    An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3

    Gloria, H. R. | NTRS | 1958
    Keywords: LONGITUDINAL STABILITY AND CONTROL

    An investigation of the dynamic stability and control characteristics for a transport cruising at a mach number of 3

    Brown, L. W. | NTRS | 1964
    Keywords: LATERAL STABILITY AND CONTROL

    An Investigation of the Effects of a Vortex-Generator Configuration on the Aerodynamic Characteristics of a 1/4-Scale Model of the X-1 Airplane (10-Percent-Thick Wing)

    Runckel, Jack F. / Henderson, James H. | NTRS | 1952
    Keywords: Aircraft Stability And Control

    An optimal guidance approximation theory

    Kelley, H. J. | NTRS | 1964
    Keywords: OPTIMAL CONTROL

    A passive gravitational attitude control system for satellites

    Paul, B. / West, J. W. / Yu, E. Y. | NTRS | 1963
    Keywords: ATTITUDE CONTROL

    Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings

    Fisher, Lewis R | NTRS | 1949
    Keywords: STABILITY & CONTROL - EFFECT OF COMPRESSIBILITY

    Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers

    Toll, Thomas A / Schneiter, Leslie E | NTRS | 1948
    Keywords: CONTROL SURFACES - HINGE MOMENTS

    A Procedure to Estimate the Size of a Suction Flap for a Passive HLFC System

    Free access
    Schrauf, Geza | German Aerospace Center (DLR) | 2022
    Keywords: Hybrid Laminar Flow Control (HLFC)

    A Small Spacecraft Swarm Deployment and Stationkeeping Strategy for Sun-Earth L1 Halo Orbits

    Conn, Tracie R. / Bookbinder, Jay A. | NTRS | 2018
    Keywords: Optimal control

    A split-damper inertially coupled passive gravity-gradient attitude control system.

    Merrick, V. K. / Tinling, B. E. / Watson, D. M. | NTRS | 1967
    Keywords: SATELLITE ATTITUDE CONTROL

    A Summary of the Cassini Spacecraft Thermal Performance from Launch through Early Cruise

    Millard, J. / Tsuyuki, G. / Clark, S. et al. | NTRS | 1998
    Keywords: control

    A Summary of the Cassini Spacecraft Thermal Performance from Launch through Early Cruise

    Millard, J. / Tsuyuki, G. / Clark, S. et al. | NTRS | 1998
    Keywords: control

    A Summary of the Cassini Spacecraft Thermal Performance from Launch Through Early Cruise

    Millard, J. / Tsuyuki, G. / Clark, S. et al. | NTRS | 1998
    Keywords: control

    A technique for optimal final value control of powered flight trajectories.

    Pfeiffer, C. G. | NTRS | 1966
    Keywords: OPTIMAL CONTROL , TRAJECTORY CONTROL

    A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit

    Barker, L. K. / Queijo, M. J. | NTRS | 1964
    Keywords: MANUAL CONTROL

    A theoretical investigation of the effect on the lateral oscillations of an airplane of an automatic control sensitive to yawing accelerations

    Beckhardt, Arnold R | NTRS | 1950
    Keywords: STABILITY & CONTROL, LATERAL

    A Theoretical Investigation of the Rolling Oscillations of an Airplane with Ailerons Free

    Cohen, Doris | NTRS | 1944
    Keywords: STABILITY & CONTROL , CONTROL SURFACES - HINGE MOMENTS

    Attitude Control System and Star Tracker Performance of the Wide-Field Infrared Explorer Spacecraft

    Lebsock, K. / Gautier, N. / Hacking, P. et al. | NTRS | 2000
    Keywords: control

    Attitude instability regions of a spinning symmetric satellite in an elliptic orbit.

    Meirovitch, L. / Wallace, F. B., Jr. | NTRS | 1967
    Keywords: SATELLITE ATTITUDE CONTROL , STABILITY AND CONTROL

    Boundary-layer and Stalling Characteristics of the NACA 63-009 Airfoil Section

    Gault, Donald E | NTRS | 1949
    Keywords: BOUNDARY LAYER CONTROL - AIRFOILS - NACA 63-009

    Boundary-layer and Stalling Characteristics of the NACA 64A006 Airfoil Section

    Mccullough, George B / Gault, Donald E | NTRS | 1949
    Keywords: BOUNDARY LAYER CONTROL - AIRFOILS - NACA 64A006

    Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

    Goranson, R Fabian | NTRS | 1942
    Keywords: STABILITY & CONTROL, LONGITUDINAL

    Calculation of control gains with filters for rigid body motion of a space vehicle

    Beutjer, W. H. | NTRS | 1966
    Keywords: SPACECRAFT CONTROL

    Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions

    Gillis, Clarence L | NTRS | 1942
    Keywords: CONTROL STICKS - FORCES

    Characteristics of Low-aspect Ratio Wings at Supercritical Mach Numbers

    Stack, John / Lindsey, W F | NTRS | 1948
    Keywords: STABILITY & CONTROL - EFFECT OF COMPRESSIBILITY

    Characteristics of thin triangular wings with constant-chord full-span control surfaces at supersonic speeds

    Tucker, Warren A | NTRS | 1948
    Keywords: CONTROL SURFACES - HINGE MOMENTS

    Characteristics of thin triangular wings with triangular-tip control surfaces at supersonic speeds with Mach lines behind the leading edge

    Tucker, Warren A | NTRS | 1948
    Keywords: CONTROL SURFACES - HINGE MOMENTS

    Characterization of DBD Plasma Actuators Performance Without External Flow - Part I: Thrust-Voltage Quadratic Relationship in Logarithmic Space for Sinusoidal Excitation

    Ashpis, David E. / Laun, Matthew C. | NTRS | 2016
    Keywords: Flow Control

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