Publications
Detailed Information
정렬비행을 위한 적응 스칼라 필터의 성능 분석 : Performance Analysis of Scalar Adaptive Filter for Formation Flying
DC Field | Value | Language |
---|---|---|
dc.contributor.author | 임준규 | - |
dc.contributor.author | 박찬국 | - |
dc.contributor.author | 이달호 | - |
dc.date.accessioned | 2009-09-20T08:27:53Z | - |
dc.date.available | 2009-09-20T08:27:53Z | - |
dc.date.issued | 2008-05 | - |
dc.identifier.citation | 한국항공우주학회지, 제36권 제5호, 2008, pp.455~461 | en |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | https://hdl.handle.net/10371/9656 | - |
dc.description.abstract | In this paper, the performance of a scalar filter and a scalar adaptive filter are anal yzed. In order to make indoor experimental environment similar to outdoor test, ultrasonic sensors are used instead of CPS. The scalar adaptive filter, which is continuously estimating velocity error covariance and measurement noise covariance by using adaptive method, is different from the scalar filter. Experimental results show that the scalar adaptive filter has better position estimating performance than the scalar filter by estimating above two parameters with an adaptive method. | en |
dc.description.sponsorship | 이 논문은 한국과학재단 특정기초연구(R01-2006-000-10189-0) 지원으로 수행되었습니다. | en |
dc.language.iso | ko | - |
dc.publisher | 한국항공우주학회 = The Korean Society for Aeronautical & Space Sciences | en |
dc.subject | 정렬비행 | en |
dc.subject | 적응 스칼라 필터 | en |
dc.subject | 이상 점프 현상 | en |
dc.subject | Formation Flying | en |
dc.subject | Scalar adaptive Filter | en |
dc.subject | Cycle slip | en |
dc.title | 정렬비행을 위한 적응 스칼라 필터의 성능 분석 | en |
dc.title.alternative | Performance Analysis of Scalar Adaptive Filter for Formation Flying | en |
dc.type | Article | en |
dc.contributor.AlternativeAuthor | Lim, Junkyu | - |
dc.contributor.AlternativeAuthor | Park, Changook | - |
dc.contributor.AlternativeAuthor | Lee, Dalho | - |
- 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.