Graduate Thesis Or Dissertation
 

Studies on attitude control of small payloads of sounding rockets

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https://ir.library.oregonstate.edu/concern/graduate_thesis_or_dissertations/4x51hn340

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  • This work has the purpose of presenting an approach to attitude control applicable for sun alignment on scientific payloads. As a primary source of information in order to obtain the alignment error signals, four solar cells are disposed about the body of the payload. As a secondary source a pair of magnetometers are used. In the development of this thesis, the author stresses some approximations useful for the sake of simplicity without compromising the results. He points out several technological aspects which are necessary for practical realization of the system. The theory of fluxgate magnetometers is discussed and a model for the simulation of the sensor is given. Every step of development presents a model for a further simulation of the system.
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  • File scanned at 300 ppi (Monochrome) using ScandAll PRO 1.8.1 on a Fi-6770A in PDF format. CVista PdfCompressor 5.0 was used for pdf compression and textual OCR.
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