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    An Overview of the NASA Test Platform Research (2003)
    In:  CASI
    Details
    Publication Date: 2018-06-05
    Description: A methodology for improving attitude stability and control for low-speed and hovering air vehicle is under development. In addition to aerodynamically induced control forces such as vector thrusting, the new approach exploits the use of bias momenta and torque actuators, similar to a class of spacecraft system, for its guidance and control needs. This approach will be validated on a free-flying research platform under development at NASA Langley Research Center. More broadly, this platform also serves as an in-house testbed for research in new technologies aimed at improving guidance and control of a Vertical Take-Off and Landing (VTOL) vehicle.
    Keywords: Aircraft Stability and Control
    Format: application/pdf
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