Publications

Detailed Information

Improvement of Attitude Estimation Using Hidden Markov Model Classification

DC Field Value Language
dc.contributor.authorKang, Chul Woo-
dc.contributor.authorPark, Chan Gook-
dc.date.accessioned2010-12-30T06:02:56Z-
dc.date.available2010-12-30T06:02:56Z-
dc.date.issued2010-04-
dc.identifier.citationAIAA Infotech@Aerospace 2010 Conference and Exhibiten
dc.identifier.urihttps://hdl.handle.net/10371/72165-
dc.description.abstractThis paper introduces the attitude estimation method of AHRS using an Extended
Kalman Filter(EKF) with a filter tuning algorithm based on Hidden Markov Model(HMM).
The AHRS uses inertial sensors and magnetometers to calculate its attitude. It is known that
the attitude update using gyros are prone to diverge and hence the attitude error needs to
compensate using accelerometers and magnetometers. In this paper, a Kalman filter model
with a state variables represented by a quaternion is presented and a model changing
algorithm is used to make the filter more robust to acceleration and magnetic disturbances.
If the AHRS measures any disturbances which are caused by movement of the vehicle,
HMM estimates the existence of disturbances. Using these estimates HMM changes the filter
gain using tuning parameters of the filter. Results of EKF tuned by HMM indicate that the
proposed method makes robust to disturbances more properly.
en
dc.description.sponsorshipDAPA/ADD/NSLen
dc.language.isoenen
dc.titleImprovement of Attitude Estimation Using Hidden Markov Model Classificationen
dc.typeConference Paperen
dc.contributor.AlternativeAuthor강철우-
dc.contributor.AlternativeAuthor박찬국-
Appears in Collections:
Files in This Item:
There are no files associated with this item.

Altmetrics

Item View & Download Count

  • mendeley

Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.

Share