Papers presented at Boston, Mass, May 25-27 1960: Command and Data Link for Astronomical Satellite L.L.ANTES 5-13; Guidance and Control Techniques for Coplanar Orbital Rendezvous, E.HARRISON, 14-20; Long-Time Satellite Rendezvous Trajectory, L.W.SPRADLIN, 21-7; Guidance and Control of Point Return Vehicles, J.H.LOWRY Jr, C.D. BUEHRLE, 28-33; Horizon Sensors for Vertical Stabilization of Satellites and Space Vehicles, M.H.ARCK, M.M.MERLEN, 34-9; Accurate Determination of Attitude by Optical Means for Application in Space Vehicles, G.von PAHLENFEDOROFF, 40-6; Application of Optical Techniques to Interplanetary Navigation, W.J.HAYWOOD Jr, 47-52; Free Reaction Sphere Satellite Attitude Control System, R.D.ORMSBY, 53-5; Magnetic Support for Floated Inertial Instruments, P.J. GILINSON Jr, W.G.DENAR D, R.H.FRAZIER, 56-83; Limit-Cycle Efficiency of on-off Reaction Control Systems, G.W. FREEMAN, 84-97; Methods of Analysis of Control System for Large Flexible Missile, D.R.LUKENS, 98-108; Pilot Control of Space Vehicle Tumbling, J.W.USELLER, J.S.ALGRANTI, 109-13; V/H Satellite Attitude Control, P.A.BUTTON, P.E. MALLORY, S.B.BOOR, 114-20; Control Development for Jet VTOL, J.A.O'MALLEY Jr, 121-9; In-Flight Measurement of Human Operator Alertness, T.B.SHERIDAN, 130-4; Design of Propulsion and Stabilization System for Man in Cosmonotic Environment, J.B.GRIFFIN, F.T.GARDNER, M.L. BARNETT, 135-44; Hovering and Longitudinal Dynamics of Ground Effect Machine with Derivations of Stability Derivatives for Vertical Motion, T.Y.FENG, 145-56; Design Principles for Control Computer for Space Guidance, R. L.ALONSO, J.H.LANING Jr, 157-66 Trajectory Problems in Cislunar Space, G.SHAPIRO, 167-77; Terminal Guidance for Lunar and Planetary Probes, R.H.GRUBE, 178-83; Differential Correction Method of Interplanetary Navigation, H.G.SAFREN, 184-90; Study of Adaptive Control System Using Digital Simulation, T.R.BENEDICT, H.R.LELAND, W. C.SCHULTZ, M.G. SPOONER, 191-6; Application of Adaptive Control Techniques to Aero/Space Vehicles, W.F.O'NEILL, M.J.ABZUG, 197-208; Method of Graphical Trajectory Analysis, A.S.BOKSENBOM, 209-21; Prediction of Anisoelastic and Vibropendulous Effects on Inertial Navigation System Performance in Linear Random Vibration Environments, S.LESHNOVER, 222-50. (Member price $5.00, nonmember price $10.00.)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    National Specialists Meeting on Guidance of Aerospace Vehicles -- Proc


    Weitere Titelangaben:

    National Specialists Meeting Guidance Aerospace Vehicles -- Proc


    Kongress:

    Proceedings of the National Specialists Meeting on Guidance of Aerospace Vehicles ; 1960 Control



    Erscheinungsdatum :

    1960


    Format / Umfang :

    250 pages


    Medientyp :

    Konferenzband


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Rendezvous guidance of lifting aerospace vehicles

    Vaccaro, R.J. / Kirby, M.J. | Engineering Index Backfile | 1965


    Automation Applications for rotorcraft : National Specialists' Meeting

    Southern Region, Atlanta Chapter, American Helicopter Society | TIBKAT | 1988


    Rotor System Design : National Specialists' Meeting ; Papers

    American Helicopter Society, Mideast Region | TIBKAT | 1980


    Rendezvous guidance of lifting aerospace vehicles

    KIRBY, M. J. / VACCARO, R. J. | AIAA | 1965