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    Approach path control for powered-lift STOL aircraft (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A flight control system concept is defined for approach flightpath control of an augmentor wing (or similar) powered-lift STOL configuration. The proposed STOL control concept produces aircraft transient and steady-state control responses that are familiar to pilots of conventional jet transports, and has potential for good handling qualities ratings in all approach and landing phases. The effects of trailing-edge rate limits, real-engine dynamics, and atmospheric turbulence are considered in the study. A general discussion of STOL handling qualities problems and piloting techniques is included.
    Keywords: AIRCRAFT
    Type: NASA-CR-114574 , D6-60222
    Format: application/pdf
    Location Call Number Expected Availability
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