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.

[img] PDF
Restricted to Repository staff only

Download (6MB)


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: Monograph (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
Depositing User: Users 64 not found.
Date Deposited: 13 Jul 2006
Last Modified: 24 May 2010 04:13
URI: http://nal-ir.nal.res.in/id/eprint/1655

Actions (login required)

View Item View Item