Extended Kalman filter with manifold state representation for navigating a maneuverable melting probe
by ,
Abstract:
We present a multi-sensor fusion approach based on an extended Kalman filter for estimating position and attitude in 3-dimensional space. The corresponding state is represented by a manifold that allows for a robust and mathematically consistent estimation of the state and uncertainty. The filter is used for navigating a maneuverable melting probe through deep ice, which is designed for in-situ sample analysis missions to icy bodies of our solar system. It is equipped with a variety of sensors for inertial navigation and absolute positioning that account for the fact that no global navigation satellite system (GNSS) can be used. The probe and navigation technologies were successfully tested on European and Antarctic glaciers. We demonstrate the performance of our algorithm and compare it to a particle filter approach in different simulated and real-world scenarios.
Reference:
Extended Kalman filter with manifold state representation for navigating a maneuverable melting probe (Joachim Clemens, Kerstin Schill), In 19th International Conference on Information Fusion (FUSION), IEEE, 2016.
Bibtex Entry:
@inproceedings{clemens2016ekf,
	author={Clemens, Joachim and Schill, Kerstin},
	title = {Extended {Kalman} filter with manifold state representation for navigating a maneuverable melting probe},
	booktitle={19th International Conference on Information Fusion (FUSION)},
	year={2016},
	month=jul,
	pages={1789--1796},
	abstract = {We present a multi-sensor fusion approach based on an extended Kalman filter for estimating position and attitude in 3-dimensional space. The corresponding state is represented by a manifold that allows for a robust and mathematically consistent estimation of the state and uncertainty. The filter is used for navigating a maneuverable melting probe through deep ice, which is designed for in-situ sample analysis missions to icy bodies of our solar system. It is equipped with a variety of sensors for inertial navigation and absolute positioning that account for the fact that no global navigation satellite system (GNSS) can be used. The probe and navigation technologies were successfully tested on European and Antarctic glaciers. We demonstrate the performance of our algorithm and compare it to a particle filter approach in different simulated and real-world scenarios.},
	publisher={IEEE},
  organization = {ISIF},
	url = {http://ieeexplore.ieee.org/document/7528100/}
}