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Tight Integration Between IMU and GPS for Sounding Rockets
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
2010 (English)Report (Other academic)
Abstract [en]

This report presents integrity monitoring and integration methods for an Inertial Measurement Unit (IMU) and a gps receiver. The methods are applied to data from a Maxus sounding rocket used for microgravity research. It is crucial to determine the rocket position during launch to ensure a safe landing location. Today, the navigation relies on IMU integration only. Involving a GPS receiver enhances the position accuracy but there is a need for protection against faulty satellite range measurements. Monitoring over a sequence of the measurements gives higher confidence to the tests.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2010. , 30 p.
Series
LiTH-ISY-R, ISSN 1400-3902 ; 2929
Keyword [en]
Integrity monitoring, Fault detection, GPS, IMU
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-97542ISRN: LiTH-ISY-R-2929OAI: oai:DiVA.org:liu-97542DiVA: diva2:648377
Available from: 2013-09-16 Created: 2013-09-16 Last updated: 2014-09-22Bibliographically approved

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fulltext(1056 kB)1904 downloads
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CiteExportLink to record
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  • apa
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