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High Performance Stepper Motors for Space MechanismsHybrid stepper motors are very well adapted to high performance space mechanisms. They are very simple to operate and are often used for accurate positioning and for smooth rotations. In order to fulfill these requirements, the motor torque, its harmonic content, and the magnetic parasitic torque have to be properly designed. Only finite element computations can provide enough accuracy to determine the toothed structures' magnetic permeance, whose derivative function leads to the torque. It is then possible to design motors with a maximum torque capability or with the most reduced torque harmonic content (less than 3 percent of fundamental). These later motors are dedicated to applications where a microstep or a synchronous mode is selected for minimal dynamic disturbances. In every case, the capability to convert electrical power into torque is much higher than on DC brushless motors.
Document ID
19950020851
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Patrick Sega
(Societe d'Applications Generales d'Electricite et de Mecanique Paris, France)
Christine Estevenon
(Societe d'Applications Generales d'Electricite et de Mecanique Paris, France)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: 29th Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Subject Category
Electronics and Electrical Engineering
Report/Patent Number
NASA/CP-3293
Meeting Information
Meeting: 29th Aerospace Mechanisms Symposium
Location: League City, TX
Country: US
Start Date: May 17, 1995
End Date: May 19, 1995
Sponsors: Lockheed Missiles and Space Company (United States), National Aeronautics and Space Administration
Accession Number
95N27271
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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