1–18 of 18 hits
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    Measures of merit for fault-tolerant systems

    GAI, E. / ADAMS, M. | AIAA | 1983

    Autonomous satellite navigation by stellar refraction

    GOUNLEY, R. / WHITE, R. / GAI, E. | AIAA | 1983

    A new approach to fault-tolerant helicopter swashplate control

    WALKER, B. / GAI, E. / DESAI, M. | AIAA | 1983

    Autonomous satellite navigation by stellar refraction

    Gounley, R. / White, R. / Gai, E. | NTRS | 1984

    A fault-tolerant approach to helicopter swashplate control

    WALKER, B. K. / GAI, E. / DESAI, M. N. | AIAA | 1985

    Use of known landmarks for satellite navigation

    WHITE, R. / GAI, E. / GRANT, F. et al. | AIAA | 1975

    The Century of Inertial Navigation Technology

    Gai, E. / Institute of Electrical and Electronics Engineers | British Library Conference Proceedings | 2000

    Finite point method: a new approach to model the inflation of side curtain airbags

    Gai,E. / Zhang,H. / ESI North America,US et al. | Automotive engineering | 2005

    FDI Performance of Two Redundant Sensor Configurations

    Gai, E. / Harrison, J. V. / Daly, K. C. | IEEE | 1979

    Decision behavior with changing signal strength

    Curry, R. E. / Gai, E. G. / Nagel, D. C. | NTRS | 1974

    Autonomous satellite navigation by stellar refraction

    GOUNLEY, R. / Charles Stark Draper Laboratory / Inc. et al. | AIAA | 1984

    Evaluation methodologies for an advanced information processing system

    SCHABOWSKY, JR., R. / GAI, E. / WALKER, B. et al. | AIAA | 1984