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   Determination of Thrust Force Ripple of a Spherical Linear PM Motor for a Direct Telescope Drive   [View] 
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 Author(s)   M. Anders; E-CH. Andresen; A. Binder 
 Abstract   A three axes torque motor consisting of several spherical shaped linear motor units for adjusting an airborne telescope is presented. An analytical calculation method for the produced thrust force of one motor unit using a tow layer chorded air gap winding is described. Calculation results are varified by test results of an existing test bench, providing the low thrust force ripple of 3% of related thrust force. 
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Filename:EPE1999 - PP00273 - Anders.pdf
Filesize:1.482 MB
 Type   Members Only 
 Date   Last modified 2004-03-25 by System