Abstract
This paper examines the problem of estimating conservative error bounds of inertial navigation systems when they are used as part of an integrated navigation system designed around a low cost inertial measurement unit (automotive/commerical grade). This is done by recasting the inertial navigation error equations for low cost sensors in a form which allows proving that the time update equations can be statistically overbounded. The resulting overbounds, however, are shown to be overly conservative.
| Original language | English (US) |
|---|---|
| Title of host publication | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 |
| Publisher | Institute of Navigation |
| Pages | 2062-2068 |
| Number of pages | 7 |
| ISBN (Electronic) | 9781634399913 |
| State | Published - 2014 |
| Event | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 - Tampa, United States Duration: Sep 8 2014 → Sep 12 2014 |
Publication series
| Name | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 |
|---|---|
| Volume | 3 |
Other
| Other | 27th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2014 |
|---|---|
| Country/Territory | United States |
| City | Tampa |
| Period | 9/8/14 → 9/12/14 |
Bibliographical note
Publisher Copyright:Copyright © (2014) by the Institute of Navigation All rights reserved.