The paper addresses the analysis of a loosely coupled Inertial/GPS navigation system suitable for small UAVs applications. In order to provide a complete solution in terms of vehicle’s attitude, velocity, and position and sensors biases two different Extended Kalman Filters (EKFs) are implemented. Mathematical description as well as numerical and experimental results are presented.
Coupled GPS/INS integration for Unmanned Aerial Vehicle Applications
GIULIETTI, FABRIZIO;
2009
Abstract
The paper addresses the analysis of a loosely coupled Inertial/GPS navigation system suitable for small UAVs applications. In order to provide a complete solution in terms of vehicle’s attitude, velocity, and position and sensors biases two different Extended Kalman Filters (EKFs) are implemented. Mathematical description as well as numerical and experimental results are presented.File in questo prodotto:
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