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Low-Cost Reaction Wheel Design for C...

Bonafede, Nicholas J., Jr.

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Low-Cost Reaction Wheel Design for Cubesat Applications.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Low-Cost Reaction Wheel Design for Cubesat Applications./
Author:	Bonafede, Nicholas J., Jr.
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2020,
Description:	163 p.
Notes:	Source: Masters Abstracts International, Volume: 85-01.
Contained By:	Masters Abstracts International85-01.
Subject:	Control algorithms. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30512890
ISBN:	9798379824402

Low-Cost Reaction Wheel Design for Cubesat Applications.
Bonafede, Nicholas J., Jr.

Low-Cost Reaction Wheel Design for Cubesat Applications. - Ann Arbor : ProQuest Dissertations & Theses, 2020 - 163 p.

Source: Masters Abstracts International, Volume: 85-01.

Thesis (M.Sc.)--California Polytechnic State University, 2020.

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

As science instruments on CubeSats become more sensitive to the attitude of the spacecraft, better methods must be employed to provide the accuracy needed to complete the planned mission. While systems that provide the accuracy required are available commercially, these solutions are not costeffective, do not allow the design to be tailored to a specific mission, and most importantly, do not give students hand-on experience with attitude control actuators. This thesis documents the design, modeling, and simulation of a lowcost, student-fabricated, reaction wheel system for use in 3U CubeSat satellites. The entire design process for the development of this reaction wheel is based on fundamental design principles and can be replicated for either larger or smaller spacecraft as needed. Additionally, plans for bringing this design up to a prototyping and testing phase are outlined for continued use of this design in the Cal Poly CubeSat Laboratory.

ISBN: 9798379824402Subjects--Topical Terms:

3560702
Control algorithms.

Low-Cost Reaction Wheel Design for Cubesat Applications.
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500 $a Source: Masters Abstracts International, Volume: 85-01.
500 $a Advisor: Murray, William R.
502 $a Thesis (M.Sc.)--California Polytechnic State University, 2020.
506 $a This item must not be sold to any third party vendors.
520 $a As science instruments on CubeSats become more sensitive to the attitude of the spacecraft, better methods must be employed to provide the accuracy needed to complete the planned mission. While systems that provide the accuracy required are available commercially, these solutions are not costeffective, do not allow the design to be tailored to a specific mission, and most importantly, do not give students hand-on experience with attitude control actuators. This thesis documents the design, modeling, and simulation of a lowcost, student-fabricated, reaction wheel system for use in 3U CubeSat satellites. The entire design process for the development of this reaction wheel is based on fundamental design principles and can be replicated for either larger or smaller spacecraft as needed. Additionally, plans for bringing this design up to a prototyping and testing phase are outlined for continued use of this design in the Cal Poly CubeSat Laboratory.
590 $a School code: 2104.
650 4 $a Control algorithms. $3 3560702
650 4 $a Gravity. $3 535300
650 4 $a Atmosphere. $3 542821
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650 4 $a Wire. $3 3681397
650 4 $a Magnetic fields. $3 660770
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650 4 $a Radiation. $3 673904
650 4 $a Ground stations. $3 3683603
650 4 $a Vehicles. $3 2145288
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Electromagnetics. $3 3173223
650 4 $a Physics. $3 516296
650 4 $a Transportation. $3 555912
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