Evaluation of linear DC motor actuators for control of large space structures

This thesis examines the use of a linear DC motor as a proof mass actuator for the control of large space structures. A model for the actuator, including the current and force compensation used, is derived. Because of the force compensation, the actuator is unstable when placed on a structure. Relat...

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Main Author: Ide, Eric Nelson
Other Authors: Electrical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/45164
http://scholar.lib.vt.edu/theses/available/etd-10132010-020121/
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-451642021-05-05T05:40:48Z Evaluation of linear DC motor actuators for control of large space structures Ide, Eric Nelson Electrical Engineering Lindner, Douglas K. Beex, A. A. Louis Bingular, Stanoje P. LD5655.V855 1988.I33 Large space structures (Astronautics) Signal processing -- Digital techniques This thesis examines the use of a linear DC motor as a proof mass actuator for the control of large space structures. A model for the actuator, including the current and force compensation used, is derived. Because of the force compensation, the actuator is unstable when placed on a structure. Relative position feedback is used for actuator stabilization. This method of compensation couples the actuator to the mast in a feedback configuration. Three compensator designs are proposed. The physical limits of the LDCM place limits on the bandwidth of the closed loop actuator. <p>A ten mode finite element model of a flexible space structure was used in simulations to examine all aspects of the actuator's performance. The performance of the actuator is compared for the three compensator designs. The actuator bandwidth is seen to be important in the actuator's effectiveness. Increasing actuator bandwidth resulted in a saturation nonlinearity in the actuator. The excitation capability of the actuator was examined to determine the authority of the actuator. The damping of the mast modes was examined to determine the effect of the feedback configuration of the actuator/mast system. Root locus techniques were used to explain changes in the vibrational modes of the structure due to the actuator compensation. Disturbance analysis was performed to quantify the effect of corrupted measurements on the purity of force generated by the actuator. Master of Science 2014-03-14T21:47:33Z 2014-03-14T21:47:33Z 1988-05-05 2010-10-13 2010-10-13 2010-10-13 Thesis Text etd-10132010-020121 http://hdl.handle.net/10919/45164 http://scholar.lib.vt.edu/theses/available/etd-10132010-020121/ OCLC# 18344693 LD5655.V855_1988.I33.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ x, 144 leaves BTD application/pdf application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic LD5655.V855 1988.I33
Large space structures (Astronautics)
Signal processing -- Digital techniques
spellingShingle LD5655.V855 1988.I33
Large space structures (Astronautics)
Signal processing -- Digital techniques
Ide, Eric Nelson
Evaluation of linear DC motor actuators for control of large space structures
description This thesis examines the use of a linear DC motor as a proof mass actuator for the control of large space structures. A model for the actuator, including the current and force compensation used, is derived. Because of the force compensation, the actuator is unstable when placed on a structure. Relative position feedback is used for actuator stabilization. This method of compensation couples the actuator to the mast in a feedback configuration. Three compensator designs are proposed. The physical limits of the LDCM place limits on the bandwidth of the closed loop actuator. <p>A ten mode finite element model of a flexible space structure was used in simulations to examine all aspects of the actuator's performance. The performance of the actuator is compared for the three compensator designs. The actuator bandwidth is seen to be important in the actuator's effectiveness. Increasing actuator bandwidth resulted in a saturation nonlinearity in the actuator. The excitation capability of the actuator was examined to determine the authority of the actuator. The damping of the mast modes was examined to determine the effect of the feedback configuration of the actuator/mast system. Root locus techniques were used to explain changes in the vibrational modes of the structure due to the actuator compensation. Disturbance analysis was performed to quantify the effect of corrupted measurements on the purity of force generated by the actuator. === Master of Science
author2 Electrical Engineering
author_facet Electrical Engineering
Ide, Eric Nelson
author Ide, Eric Nelson
author_sort Ide, Eric Nelson
title Evaluation of linear DC motor actuators for control of large space structures
title_short Evaluation of linear DC motor actuators for control of large space structures
title_full Evaluation of linear DC motor actuators for control of large space structures
title_fullStr Evaluation of linear DC motor actuators for control of large space structures
title_full_unstemmed Evaluation of linear DC motor actuators for control of large space structures
title_sort evaluation of linear dc motor actuators for control of large space structures
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/45164
http://scholar.lib.vt.edu/theses/available/etd-10132010-020121/
work_keys_str_mv AT ideericnelson evaluationoflineardcmotoractuatorsforcontroloflargespacestructures
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