1–20 von 37 Ergebnissen
|

    Approximate optimal atmospheric entry trajectories.

    SPEYER, J. L. / WOMBLE, M. E. | AIAA | 1971

    Periodic optical cruise of an atmospheric vehicle

    SPEYER, J. L. / DANNEMILLER, D. / WALKER, D. | AIAA | 1985

    Assumed density filter with application to homing missile guidance

    BALAKRISHNAN, S. N. / SPEYER, J. L. | AIAA | 1989

    Approximate Optimal Atmospheric Entry Trajectories

    Speyer, J. L. / Womble, E. | NTRS | 1971

    Linear-quadratic guidance law for dual control of homing missiles

    HULL, D. G. / SPEYER, J. L. / BURRIS, D. B. | AIAA | 1990

    Approximate Optimal Guidance for Aerospace Systems (AAS 94-070)

    Speyer, J. L. / American Astronautical Society | British Library Conference Proceedings | 1994

    Maximum-information guidance for homing missiles

    HULL, D. G. / SPEYER, J. L. / TSENG, C. Y. | AIAA | 1985

    Control of Satellite Clusters in Elliptic Orbit with Limited Communication

    Chichka, D. F. / Belanger, G. / Speyer, J. L. | British Library Conference Proceedings | 2004

    Adaptive noise estimation for homing missiles

    HULL, D. G. / SPEYER, J. L. / GREENWELL,W. M. | AIAA | 1984

    Minimum energy-loss guidance for aeroassisted orbital plane change

    HULL, D. G. / GILTNER, J. M. / SPEYER, J. L. et al. | AIAA | 1985

    Control of Dynamic Systems in Spatial Networks: Applications, Results, and Challenges

    Speyer, J. L. / International Federation of Automatic Control | British Library Conference Proceedings | 1999

    Estimation enhancement by trajectory modulation for homing missiles

    SPEYER, J. L. / HULL, D. G. / LARSON, S.W. et al. | AIAA | 1984

    Multi-input/multi-output controller design for longitudinal decoupled aircraft motion

    SPEYER, J. L. / WHITE, J. E. / DOUGLAS, R. et al. | AIAA | 1984