This report describes the following research tasks: The test and evaluation of a quadruplex redundant Pitch Axis Test Rig (PATR) to fully describe the hydraulic, mechanical and electronic technology contained therein; and the design of a Roll Axis Test Rig (RATR) to permit hardware simulation of quad redundant, force sharing, active standby, median select and split surface flight control system mechanizations that have high dynamic response.


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    Title :

    Flight Control Actuator System Development


    Contributors:

    Publication date :

    1974


    Size :

    226 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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