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    The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: An analytical study has been made to assess the loads developed on the horizontal tail of an autopilot-controlled rigid airplane flying in one-dimensional atmospheric turbulence. The root-mean-square values of rigid-airframe responses and tail-load responses were calculated at five flight conditions, and the behavior of these responses was observed in two autopilot modes: pitch-attitude-hold mode and altitude-control mode. It was found that pitch attitude and altitude can be controlled by the simple autopilot with acceptable or no increases in tail loads.
    Keywords: AIRCRAFT
    Type: NASA-TN-D-7231 , L-8756
    Format: application/pdf
    Location Call Number Expected Availability
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