1–20 von 952 Ergebnissen
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    Research on radiational active thermal control technology for spacecraft

    ZHANG, Z. / GUO, S. / SUN, Y. et al. | AIAA | 1980

    A locked azimuth-gimbal method of INS initialization

    Ren, S. / Guo, Z.L. / Hung, J.C. | Tema Archiv | 1985

    The Intercooled-Supercharging Gas Turbine Engine

    Wang, L. S. / Guo, X. D. | SAE Technical Papers | 1989

    Analysis and Development of a Total Energy Control System for a Large Transport Aircraft

    Guo, S. F. / Wu, S. F. / Shen, Y. Z. | British Library Online Contents | 1992

    ICAS-92-2.9.3 Analysis and Development of a Total Energy Control System for a Large Transport Aircraft

    Guo, S. F. / Wu, S. F. / Shen, Y. Z. et al. | British Library Conference Proceedings | 1992

    Low Cost, Multifunctional Sensor for Vehicle's Inertial Navigation System

    Guo-Wei, G. / Ya-Hua, L. / Canadian Society for Mechanical Engineering | British Library Conference Proceedings | 1992
    Beteiligte: Sankar, S.

      Low Cost, Multifunctional Sensor for Vehicle's Inertial Navigation System

      Guo-Wei, G. / Ya-Hua, L. / Canadian Society for Mechanical Engineering | British Library Conference Proceedings | 1992
      Beteiligte: Sankar, S.

    Development of model-following idle speed control system incorporating engine torque models

    Watanabe,S. / Imamura,M. / Tomisawa,N. et al. | Kraftfahrwesen | 1992

    93ME066 DDS Framework for Automotive Vision Systems

    Pandit, S. M. / Guo, R. / Joshi, G. A. et al. | British Library Conference Proceedings | 1993

    Aeroelastic optimization of high aspect ratio wings using an exact dynamic stiffness matrix method

    Lillico, M. / Butler, R. / Banerjee, J. et al. | AIAA | 1994

      Aeroelastic Optimization of High Aspect Ratio Wings Using an Exact Dynamic Stiffness Matrix Method

      Lillico, M. / Butler, R. / Banerjee, J. et al. | British Library Conference Proceedings | 1994

    Research and Development on the Parameterized Aeroengine Structural Scheme Design System

    Guo, S. / Beijing University of Aeronautics and Astronautics | British Library Conference Proceedings | 1994

    Optimum Flight Trajectory Guidance Based on Total Energy Control of Aircraft

    Wu, S.-F. | Online Contents | 1994
    Beteiligte: Guo, S.-F.

    The Design of Inertia Platform with Reverse Frame Normalizing Theory

    Li, D. / Guo, S. / Tian, Z. et al. | British Library Conference Proceedings | 1994

    The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment

    Wu, S. / Guo, S. / United States et al. | British Library Conference Proceedings | 1994

    The Advantage of Singular Value Decomposition Used in System Identification-Data Analysing About Navigational Gyro Drift

    Tian, Z. / Guo, S. / Zhao, X. et al. | British Library Conference Proceedings | 1994