Abstract
As a result of the development of modern vehicles, even higher accuracy standards are demanded. As known, Inertial Navigation Systems have an intrinsic increasing error which is the main reason of using integrating navigation systems, where some other sources of measurements are utilized, such as barometric altimeter due to its high accuracy in short times of interval. Using a Robust Adaptive Kalman Filter (RAKF), error measurements are absorbed when a Fault Tolerant Altimeter is implemented. During simulations, in order to test the Nonlinear RAKF algorithm, two kind of measurement fault scenarios are examined; continuous bias and measurement noise increment. Under the light of the results, some recommendations are proposed when integrated altimeters are used.
Original language | English |
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Title of host publication | Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019 |
Editors | Andrzej Kot, Agata Nawrocka |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
ISBN (Electronic) | 9781728107011 |
DOIs | |
Publication status | Published - May 2019 |
Event | 20th International Carpathian Control Conference, ICCC 2019 - Krakow - Wieliczka, Poland Duration: 26 May 2019 → 29 May 2019 |
Publication series
Name | Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019 |
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Conference
Conference | 20th International Carpathian Control Conference, ICCC 2019 |
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Country/Territory | Poland |
City | Krakow - Wieliczka |
Period | 26/05/19 → 29/05/19 |
Bibliographical note
Publisher Copyright:© 2019 IEEE.
Keywords
- Adaptive estimation
- Barometric altimeter
- GPS
- Inertial navigation
- Integrated altimeter
- Kalman filter
- Robust filter