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    The Effects of Propellant Slosh Dynamics on the Solar Dynamics Observatory

    Mason, P. / Starin, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The effect of haptic guidance on curve negotiation behavior of young, experienced drivers

    Mulder, M. / Abbink, D.A. / Boer, E.R. | Tema Archiv | 2008
    guidance based on the concept of shared control, where both the driver and the support system influence the steering wheel torque. The haptic ...

    The Effect of Faster Engine Response on the Lateral Directional Control of a Damaged Aircraft

    May, R. / Lemon, K. / Csank, J. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The Effect of Explicit Adaptive Time Delay Compensation on Time Delay Margin

    Yildiz, Y. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The dynamic modeling of hysteresis and application to damping of spacecraft librations

    ANAND, D. / PISACANE, V. | AIAA | 1969
    Verlag: The American Institute of Aeronautics and Astronautics

    The dynamic infrared missile evaluator (DIME) and electro-optical signature analysis system (EOSAS) facilities

    Vogel, G.A. / Huber, E.G. | Tema Archiv | 1990
    flare and jammer techniques on actual missile guidance and control units under real-time dynamic fly-out conditions. The second facility, called ...
    Schlagwörter: MISSILE GUIDANCE

    The Design of Urban Parking Guidance and Information System Based on ZigBee Technology

    Huang, Cheng-Kai / Cui, Xiao-Yan / Li, Yao-Kai et al. | Tema Archiv | 2013
    This paper proposes a complete set of Urban Parking Guidance and Information System, which includes Parking Subsystem and City Parking ...

    The Design of Polynomial Eigenstructure Assignment Controller and Its Robust Analysis for Flexible Spacecraft Precise Control System

    Wang, F. / Ankersen, F. / Tsourdos, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The CryoSat AOCS - A Cost-Efficient Design for Small Earth Observation Satellites

    Usbeck, T. / European Space Agency | British Library Conference Proceedings | 2003
    Schlagwörter: spacecraft guidance , control systems

    The century of inertial navigation technology

    Gai, E. | IEEE | 2000
    In the early 1930's, visionary engineers and scientists began thinking about practical self-contained systems for the guidance, navigation ...

    The Artemis Satellite Unexpected Trip to GEO Orbit

    Mazzini, L. / Tamilia, V. / European Space Agency | British Library Conference Proceedings | 2003
    Schlagwörter: spacecraft guidance , control systems

    The APS Based Smart Sun Sensor Ready for the Market

    Boldrini, F. / European Space Agency | British Library Conference Proceedings | 2003
    Schlagwörter: spacecraft guidance , control systems

    The Application of MEMS Gyroscope in Stable Platform of Infrared Guidance

    Ren, Ya-Fei / Ge, Yun-Wang / Bai, Xu-Can | Tema Archiv | 2012
    In recent years, Gyro stabilized and tracking platform has been widely used in the guidance, airborne, ship-borne, the military area and ...

    The Applicability of Unsteady Vortex Panel Methods to the Design of Hovering Flapping-Wing Micro Air Vehicles

    Prosser, D. / Crassidis, A. / Ghosh, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The AOCS Framework

    Cechticky, V. / European Space Agency | British Library Conference Proceedings | 2003
    Schlagwörter: spacecraft guidance , control systems

    Test results for an off the shelf GPS/INS during approach and landing testing of the X-40A

    Childers, D. / Gelderloos, H. | Tema Archiv | 2001
    autonomously. At the heart of the Guidance, Navigation and Control (GN&C) will be the Space Integrated GPS/INS (SIGI) system, an off the shelf ...

    Testing Operating Procedures for Large UAS with Detect and Avoid Capabilities in Civil Air Traffic Management Environments

    Bleakley, Timothy / Sunil, Emmanuel | IEEE | 2023
    -fidelity Air Traffic Control (ATC) simulation facility to provide professional controllers and pilots with the experience of introducing large UAS ...

    Testing of the Lunar Reconnaissance Orbiter Attitude Control System Re-Design Without a Gyro

    Halverson, Julie / Calhoun, Phil / Hsu, Oscar et al. | NTRS | 2019
    observe various sciencetargets. LRO attitude control system (ACS) has two star trackers and a gyro forattitude estimation in an extended Kalman ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance

    Testing of RTK-level satellite-based tractor auto- guidance using a visual sensor system

    Easterley, Dwight / Adamchuk, Viacheslav / Hoy, Roger et al. | Tema Archiv | 2010
    include the automated steering of tractors and self-propelled machinery. With the development of auto-guidance systems comes the need to evaluate ...

    Testing of Immunity-Based Failure Detection and Identification Scheme with the NASA Generic Transport Model

    Perhinschi, M. / Moncayo, H. / Wilburn, B. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

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