Microprocessor based controller for actuators in structural testing

Sunder, R and Venkatesh, CS (1992) Microprocessor based controller for actuators in structural testing. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Full-scale and component testing of airframes requires13; synchronised loading and control of multiple actuators13; through real time computers. Conventional test controllers use analog link between the controller and the actuator. This report describes an attempt at developing a digital link between the host computer and controllers mounted on individual actuators.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Full-scale;Component testing;Multiple actuator controllers; Digital analog links;Host computer
    Subjects: ENGINEERING > Structural Mechanics
    AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Structures Division, Structures Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 13 Jul 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1655

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