國立虎尾科技大學 |

Low-Cost Reaction Wheel Design for Cubesat Applications.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Low-Cost Reaction Wheel Design for Cubesat Applications./
作者:	Bonafede, Nicholas J., Jr.
面頁冊數:	1 online resource (163 pages)
附註:	Source: Masters Abstracts International, Volume: 85-01.
Contained By:	Masters Abstracts International85-01.
標題:	Control algorithms. -
電子資源:	click for full text (PQDT)
ISBN:	9798379824402

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

Low-Cost Reaction Wheel Design for Cubesat Applications. - 1 online resource (163 pages)

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

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

Includes bibliographical references

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.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798379824402Subjects--Topical Terms:

1372652
Control algorithms.
Index Terms--Genre/Form:

554714
Electronic books.

Low-Cost Reaction Wheel Design for Cubesat Applications.
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500 $a Advisor: Murray, William R.
502 $a Thesis (M.Sc.)--California Polytechnic State University, 2020.
504 $a Includes bibliographical references
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.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2024
538 $a Mode of access: World Wide Web
650 4 $a Control algorithms. $3 1372652
650 4 $a Gravity. $3 591794
650 4 $a Atmosphere. $3 670485
650 4 $a Spacecraft. $3 1437734
650 4 $a Wire. $3 1437735
650 4 $a Magnetic fields. $3 598365
650 4 $a Sensors. $3 1003702
650 4 $a Altitude. $3 1372605
650 4 $a Controllers. $3 995759
650 4 $a Design. $3 595500
650 4 $a Communications satellites. $3 1437736
650 4 $a Wheels. $3 1437737
650 4 $a Radiation. $3 673044
650 4 $a Ground stations. $3 1437738
650 4 $a Vehicles. $3 721652
650 4 $a Aerospace engineering. $3 686400
650 4 $a Electromagnetics. $3 1178899
650 4 $a Physics. $3 564049
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