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Multiple degree-of-freedom force and moment measurement for static propulsion testing using magnetic suspension technologyInnovative Information Systems (IIS), Inc. is in the process of designing and fabricating a high bandwidth force and moment measuring device (i.e. the Magnetic Thruster Test Stand). This device will use active magnetic suspension to allow direct measurements of the forces and torques generated by the rocket engines of the missile under test. The principle of operation of the Magnetic Thruster Test Stand (MTTS) is based on the ability to perform very precise, high bandwidth force and position measurements on an object suspended in a magnetic field. This ability exists due to the fact that the digital servo control mechanism that performs the magnetic suspension uses high bandwidth (10 kHz) position data (via an eddy-current proximity sensor) to determine the amount of force required to maintain stable suspension at a particular point. This force is converted into required electromagnet coil current, which is then output to a current amplifier driving the coils. A discussion of how the coil current and magnetic gap distance (the distance between the electromagnet and the object being suspended) is used to determine the forces being applied from the suspended assembly is presented.
Document ID
19930018377
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stuart, Keith
(Aura Systems, Inc. Los Angeles, CA, United States)
Bartosh, Blake
(Aura Systems, Inc. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Magnetic Suspension Technology Workshop
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
93N27566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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