the INS systems, from the first realizations on, have enjoyed a strong push to miniaturization. On the one hand, this has made them less prone to various mechanical-electrical problems and therefore reduced many of the errors due to technology. On the other hand, the intrinsic errors due to the inseparable error of the instrument remains. This paper examines a simple methodology for filtering and deleting the propagation errors of the INS systems. Most of the errors that can be mathematically compensated through an appropriate series of Kalman’s filters.
Petritoli, E., Leccese, F., Leccisi, M. (2019). Inertial navigation systems for UAV: Uncertainty and error measurements. In 2019 IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2019 - Proceedings (pp.218-222). Institute of Electrical and Electronics Engineers Inc. [10.1109/MetroAeroSpace.2019.8869618].
Inertial navigation systems for UAV: Uncertainty and error measurements
Petritoli E.;Leccese F.
;Leccisi M.
2019-01-01
Abstract
the INS systems, from the first realizations on, have enjoyed a strong push to miniaturization. On the one hand, this has made them less prone to various mechanical-electrical problems and therefore reduced many of the errors due to technology. On the other hand, the intrinsic errors due to the inseparable error of the instrument remains. This paper examines a simple methodology for filtering and deleting the propagation errors of the INS systems. Most of the errors that can be mathematically compensated through an appropriate series of Kalman’s filters.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
