The Design and Simulated Performance of the Attitude Determination and Control System of a Gravity Gradient Stabilized Cube Satellite
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The Design and Simulated Performance of the Attitude Determination and Control System of a Gravity Gradient Stabilized Cube Satellite (2015)
EN NW EB DLISBN: 9781329356412 bzw. 1329356411, in Englisch, 124 Seiten, Lulu.com, neu, E-Book, elektronischer Download.
Lieferung aus: Vereinigte Staaten von Amerika, ebook for download, Free shipping.
This is a master’s project report submitted to the mechanical engineering department of the University of Hawaiʻi at Mānoa. It discusses the design and simulated performance of the Attitude Determination and Control Subsystem of a 3U cube satellite named Hoʻoponopono (H2). H2 was developed at the UH Mānoa College of Engineering’s Small-Satellite Laboratory. Its mission was to aid in the radar calibration process of U.S. Air Force radar stations by providing a calibration source in orbit. Its gravity-gradient ADCS was designed to point H2 in the nadir direction for the entirety of its mission lifetime. The unique issues associated with achieving gravity-gradient stabilization is discussed. To ensure that the functionality and performance requirements were satisfied, the Nanosatellite Attitude Dynamics & Determination Simulator (NADDS) was developed and used to determine the energies and times required for H2 to achieve nadir pointing. Kindle Edition, Format: Kindle eBook, Label: Lulu.com, Lulu.com, Product group: eBooks, Published: 2015-07-09, Release date: 2015-07-09, Studio: Lulu.com.
This is a master’s project report submitted to the mechanical engineering department of the University of Hawaiʻi at Mānoa. It discusses the design and simulated performance of the Attitude Determination and Control Subsystem of a 3U cube satellite named Hoʻoponopono (H2). H2 was developed at the UH Mānoa College of Engineering’s Small-Satellite Laboratory. Its mission was to aid in the radar calibration process of U.S. Air Force radar stations by providing a calibration source in orbit. Its gravity-gradient ADCS was designed to point H2 in the nadir direction for the entirety of its mission lifetime. The unique issues associated with achieving gravity-gradient stabilization is discussed. To ensure that the functionality and performance requirements were satisfied, the Nanosatellite Attitude Dynamics & Determination Simulator (NADDS) was developed and used to determine the energies and times required for H2 to achieve nadir pointing. Kindle Edition, Format: Kindle eBook, Label: Lulu.com, Lulu.com, Product group: eBooks, Published: 2015-07-09, Release date: 2015-07-09, Studio: Lulu.com.
2
The Design and Simulated Performance of the Attitude Determination and Control System of a Gravity Gradient Stabilized Cube Satell
EN NW EBISBN: 9781329356412 bzw. 1329356411, in Englisch, Lulu.com, neu, E-Book.
Lieferung aus: Vereinigte Staaten von Amerika, In Stock.
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Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
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