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What is INS/GPS State Estimation for MAVs about?

This document discusses state estimation techniques for micro air vehicles using inertial sensors. It proposes using an inertial measurement system consisting of MEMS gyroscopes, accelerometers, magnetometers, and GPS integrated with three extended Kalman filter schemes for state estimation. The mathematical models and relationships used in the filters are described. A flight simulator was used to record trajectory data which was then analyzed in MATLAB simulations to evaluate the performance of the differe

Author

Arturo Rawr

Language

EN