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Three-dimensional tracking using on-board measurements

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dc.contributor.author Rekkas, CM en
dc.contributor.author Lefas Chris, C en
dc.contributor.author Krikelis, NJ en
dc.date.accessioned 2014-03-01T01:08:12Z
dc.date.available 2014-03-01T01:08:12Z
dc.date.issued 1991 en
dc.identifier.issn 0018-9251 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/10329
dc.subject System Modeling en
dc.subject Three Dimensional en
dc.subject Tracking System en
dc.subject First Order en
dc.subject kalman filter en
dc.subject.classification Engineering, Aerospace en
dc.subject.classification Engineering, Electrical & Electronic en
dc.subject.classification Telecommunications en
dc.subject.other Aircraft - Radar Equipment en
dc.subject.other Mathematical Transformations - Laplace Transforms en
dc.subject.other Radar - Tracking en
dc.subject.other Signal Filtering and Prediction - Kalman Filtering en
dc.subject.other Attitude Measurement Filter en
dc.subject.other Extended Kalman Filter en
dc.subject.other On-Board Measurements en
dc.subject.other Three-Dimensional Tracking en
dc.subject.other Air Transportation en
dc.title Three-dimensional tracking using on-board measurements en
heal.type journalArticle en
heal.identifier.primary 10.1109/7.85034 en
heal.identifier.secondary http://dx.doi.org/10.1109/7.85034 en
heal.language English en
heal.publicationDate 1991 en
heal.abstract The development of a three-dimensional tracker using onboard measurements is described. A system model based on aircraft dynamics is derived. A full 3-D tracking system that can be split, with a part operating onboard and a part operating on the ground, is developed. Attitude angle and aircraft airspeed measurements are processed to estimate the components of the aircraft velocity with respect to the surrounding air. These are then used to obtain estimates of the aircraft position and ground speed. The tracker is designed so that the number of quantities transmitted to the ground station is kept to a minimum. The tracker was evaluated with real data and was found to perform well, resulting in a considerable improvement over the conventional first-order Kalman filter. en
heal.publisher IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC en
heal.journalName IEEE Transactions on Aerospace and Electronic Systems en
dc.identifier.doi 10.1109/7.85034 en
dc.identifier.isi ISI:A1991GB87400004 en
dc.identifier.volume 27 en
dc.identifier.issue 4 en
dc.identifier.spage 617 en
dc.identifier.epage 624 en


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