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Design and Demonstration of Helmholt...

Stromecki, Michael Anthony.

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Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat./
作者:	Stromecki, Michael Anthony.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2023,
面頁冊數:	83 p.
附註:	Source: Masters Abstracts International, Volume: 85-06.
Contained By:	Masters Abstracts International85-06.
標題:	Aerospace engineering. -
電子資源:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30816370
ISBN:	9798381112665

Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat.
Stromecki, Michael Anthony.

Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat. - Ann Arbor : ProQuest Dissertations & Theses, 2023 - 83 p.

Source: Masters Abstracts International, Volume: 85-06.

Thesis (M.S.)--San Diego State University, 2023.

Attitude Determination and Control Systems (ADCS) testbeds are an important platform for the demonstration of satellite control systems prior to a satellite launch and on-orbit operations. These Earthbound testbeds may utilize an altered and controllable magnetic field, a Sun simulator, imitation star fields, air bearings, balancing weights, vacuum and temperature chambers and other mechanisms to best replicate the environment of space here on the ground. Satellites will use an array of sensors and actuators to detect and interact with their environment, their location and orientation in that environment. A CubeSat is a nanosatellite standard developed to be more affordable, more approachable, more modular, have a low barrier to entrance and have a faster turn around time alternative to traditional satellites. Many of which may weigh several tons and cost millions of dollars to test and put in space. As such, many institutions seek to use the small 10 cm, 1.3 kg modular cube standard to demonstrate their equipment or control algorithms and investigate new theories in the lab rather than in space. Thus providing great savings in time and money and allowing for greater flexibility for those wishing to test or to train students. This testbed will demonstrate effective control of a CubeSat through the use of Helmholtz coils, magnetic torquer solenoids, reaction wheels and inexpensive student-made components and available components off the shelf (COTS) in the San Diego State University SPACE Lab.

ISBN: 9798381112665Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Traditional satellites

Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat.
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245 1 0 $a Design and Demonstration of Helmholtz Coils ADCS Testbed With a Magnetorquer Actuated CubeSat.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2023
300 $a 83 p.
500 $a Source: Masters Abstracts International, Volume: 85-06.
500 $a Advisor: Bani Younes, Ahmad.
502 $a Thesis (M.S.)--San Diego State University, 2023.
520 $a Attitude Determination and Control Systems (ADCS) testbeds are an important platform for the demonstration of satellite control systems prior to a satellite launch and on-orbit operations. These Earthbound testbeds may utilize an altered and controllable magnetic field, a Sun simulator, imitation star fields, air bearings, balancing weights, vacuum and temperature chambers and other mechanisms to best replicate the environment of space here on the ground. Satellites will use an array of sensors and actuators to detect and interact with their environment, their location and orientation in that environment. A CubeSat is a nanosatellite standard developed to be more affordable, more approachable, more modular, have a low barrier to entrance and have a faster turn around time alternative to traditional satellites. Many of which may weigh several tons and cost millions of dollars to test and put in space. As such, many institutions seek to use the small 10 cm, 1.3 kg modular cube standard to demonstrate their equipment or control algorithms and investigate new theories in the lab rather than in space. Thus providing great savings in time and money and allowing for greater flexibility for those wishing to test or to train students. This testbed will demonstrate effective control of a CubeSat through the use of Helmholtz coils, magnetic torquer solenoids, reaction wheels and inexpensive student-made components and available components off the shelf (COTS) in the San Diego State University SPACE Lab.
590 $a School code: 0220.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Remote sensing. $3 535394
653 $a Traditional satellites
653 $a Control algorithms
653 $a Magnetic torquer solenoids
653 $a Helmholtz coils
653 $a Air bearings
690 $a 0538
690 $a 0799
710 2 $a San Diego State University. $b Aerospace Engineering. $3 3428806
773 0 $t Masters Abstracts International $g 85-06.
790 $a 0220
791 $a M.S.
792 $a 2023
793 $a English
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30816370