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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Tornqvist, D. Helmersson, A. Gustafsson, F. |
| Copyright Year | 2010 |
| Description | Author affiliation: Division of Automatic Control, Department of Electrical Engineering, Linköping University, SE-581 83, Sweden (Tornqvist, D.; Helmersson, A.; Gustafsson, F.) |
| Abstract | This paper presents an integrity monitoring method for tight integration of an Inertial Measurement Unit (IMU) and a GPS receiver. The method is 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. |
| Starting Page | 1 |
| Ending Page | 7 |
| File Size | 478177 |
| Page Count | 7 |
| File Format | |
| ISBN | 9781424438877 |
| ISSN | 1095323X |
| DOI | 10.1109/AERO.2010.5446730 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2010-03-06 |
| Publisher Place | USA |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Global Positioning System Acoustic testing Rockets Satellites Monitoring Azimuth Time measurement Vehicle dynamics Automatic testing Automatic control |
| Content Type | Text |
| Resource Type | Article |
| Subject | Aerospace Engineering Space and Planetary Science |
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