IMPROVED STRAPDOWN CONING ALGORITHMS
| dc.citation.epage | 490 | en_US |
| dc.citation.issue | 2 | en_US |
| dc.citation.spage | 484 | en_US |
| dc.citation.volume | 28 | en_US |
| dc.citation.woscount | 21 | |
| dc.contributor.author | JIANG, YF | en_US |
| dc.contributor.author | LIN, YP | en_US |
| dc.contributor.department | 電控工程研究所 | zh_TW |
| dc.contributor.department | Institute of Electrical and Control Engineering | en_US |
| dc.date.accessioned | 2014-12-08T15:04:57Z | |
| dc.date.available | 2014-12-08T15:04:57Z | |
| dc.date.issued | 1992-04-01 | en_US |
| dc.description.abstract | Three improved algorithms for strapdown attitude computation utilizing accumulated gyro increments from the previous and current update are developed and evaluated analytically under classical coning motion. The error criterion of Miller [6] is now derived directly from the rotation vector concept. The accuracy of updating rotation vector estimation can be improved at least two orders of magnitude as compared with those of conventional algorithms. The proposed algorithm is equivalent to increasing the number of gyro samples used in the conventional method and it requires less computer loading also. | en_US |
| dc.identifier.doi | 10.1109/7.144574 | en_US |
| dc.identifier.issn | 0018-9251 | en_US |
| dc.identifier.journal | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | en_US |
| dc.identifier.uri | http://dx.doi.org/10.1109/7.144574 | en_US |
| dc.identifier.uri | https://ir.lib.nycu.edu.tw/handle/11536/3470 | |
| dc.identifier.wosnumber | WOS:A1992JC43100017 | |
| dc.language.iso | en_US | en_US |
| dc.title | IMPROVED STRAPDOWN CONING ALGORITHMS | en_US |
| dc.type | Article | en_US |