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Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion./
Author:	Jindani, Amsal.
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2021,
Description:	80 p.
Notes:	Source: Masters Abstracts International, Volume: 83-06.
Contained By:	Masters Abstracts International83-06.
Subject:	Aerospace engineering. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28652141
ISBN:	9798496544733

Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion.
Jindani, Amsal.

Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion. - Ann Arbor : ProQuest Dissertations & Theses, 2021 - 80 p.

Source: Masters Abstracts International, Volume: 83-06.

Thesis (M.A.S.)--University of Toronto (Canada), 2021.

This item must not be sold to any third party vendors.

This thesis covers the development and simulation based implementation of a control law used to concurrently control the vibration and attitude of a square solar sail using dual gimballed corner-attached reflective vane actuators. An introduction to the topic is presented along with the prerequisite mathematical foundation needed to follow the thesis. Following that, a flexible structural dynamics model of the solar sail is developed using a Rayleigh-Ritz expansion to model the coupled rotational and elastic dynamics of the system. Next, a control law is developed using Lyapunov control design to concurrently damp structural vibrations as well as reorient the sail to a desired attitude. Subsequently, a control allocation process is presented to tackle the underconstrained nature of the tip vane actuators such that desired control forces can be realized as closely as possible. Finally, simulation results using the control law with the structural dynamics model are presented to demonstrate the improvement in vibration damping using the augmented PD control law developed as opposed to a simple PD control law.

ISBN: 9798496544733Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Attitude control

Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion.
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020 $a 9798496544733
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035 $a AAI28652141
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100 1 $a Jindani, Amsal. $0 (orcid)0000-0002-9340-982X $3 3686928
245 1 0 $a Vibration and Attitude Control of Square Solar Sails Using Tip Vane Null Motion.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2021
300 $a 80 p.
500 $a Source: Masters Abstracts International, Volume: 83-06.
500 $a Advisor: Damaren, Christopher J.
502 $a Thesis (M.A.S.)--University of Toronto (Canada), 2021.
506 $a This item must not be sold to any third party vendors.
520 $a This thesis covers the development and simulation based implementation of a control law used to concurrently control the vibration and attitude of a square solar sail using dual gimballed corner-attached reflective vane actuators. An introduction to the topic is presented along with the prerequisite mathematical foundation needed to follow the thesis. Following that, a flexible structural dynamics model of the solar sail is developed using a Rayleigh-Ritz expansion to model the coupled rotational and elastic dynamics of the system. Next, a control law is developed using Lyapunov control design to concurrently damp structural vibrations as well as reorient the sail to a desired attitude. Subsequently, a control allocation process is presented to tackle the underconstrained nature of the tip vane actuators such that desired control forces can be realized as closely as possible. Finally, simulation results using the control law with the structural dynamics model are presented to demonstrate the improvement in vibration damping using the augmented PD control law developed as opposed to a simple PD control law.
590 $a School code: 0779.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Applied physics. $3 3343996
650 4 $a Computational physics. $3 3343998
653 $a Attitude control
653 $a Control allocation
653 $a Control systems
653 $a Solar sails
653 $a Structural dynamics
653 $a Vibration control
690 $a 0538
690 $a 0215
690 $a 0216
710 2 $a University of Toronto (Canada). $b Aerospace Science and Engineering. $3 2105951
773 0 $t Masters Abstracts International $g 83-06.
790 $a 0779
791 $a M.A.S.
792 $a 2021
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28652141