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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Abstract
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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