Publications
Detailed Information
자세 비교를 통한 초소형 비행체의 자세 추정 기법 : Attitude Estimation Method through Attitude Comparison for Micro Aerial Vehicle
DC Field | Value | Language |
---|---|---|
dc.contributor.author | 임종남 | - |
dc.contributor.author | 박찬국 | - |
dc.date.accessioned | 2009-09-20T08:58:32Z | - |
dc.date.available | 2009-09-20T08:58:32Z | - |
dc.date.issued | 2006-08 | - |
dc.identifier.citation | 한국항공우주학회지, 제34권 제8호, 2006, pp.63~70 | en |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | https://hdl.handle.net/10371/9664 | - |
dc.description.abstract | Due to the small size and weight of micro aerial vehicle (MAV), only miniaturized
MEMS type sensors are applicable for MAV autonomous flight system. In this paper, we propose a accelerometer and gyro mixing algorithm to improve an attitude performance of MEMS type sensors. The performance of the proposed mixing algorithm is compared with the performance of fuzzy-based mixing algorithm through simulation. The simulation results show that the attitude compensation method through the attitude compensation has better performance than the fuzzy-based mixing method for MAV attitude estimation. | en |
dc.description.sponsorship | 본 연구는 한국과학재단 특정기초연구과제(R01-2002-000-00329-0)의 일부로 수행된 결과이며 이에 감사드립니다. | en |
dc.language.iso | ko | - |
dc.publisher | 한국항공우주학회 = The Korean Society for Aeronautical & Space Sciences | en |
dc.subject | 초소형 비행체 | en |
dc.subject | MEMS 센서 | en |
dc.subject | 가속도계 및 자이로 혼합 알고리즘 | en |
dc.subject | Micro air vehicle | en |
dc.subject | MEMS sensor | en |
dc.subject | accelerometer & gyro mixing algorithm | en |
dc.title | 자세 비교를 통한 초소형 비행체의 자세 추정 기법 | en |
dc.title.alternative | Attitude Estimation Method through Attitude Comparison for Micro Aerial Vehicle | en |
dc.type | Article | en |
dc.contributor.AlternativeAuthor | Lim, Jong-nam | - |
dc.contributor.AlternativeAuthor | Park, Changook | - |
- Appears in Collections:
- Files in This Item:
- There are no files associated with this item.
Item View & Download Count
Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.