Pitch and roll attitude estimation of a small-scaled helicopter using single antenna GPS with gyroscopes-Reference-Cited by-同舟云学术

Pitch and roll attitude estimation of a small-scaled helicopter using single antenna GPS with gyroscopes

Published:2009-01-17 Issue:3 Volume:13 Page:209-220
ISSN:1080-5370
Container-title:GPS Solutions
language:en
Short-container-title:GPS Solut

Author:

Tenn Hian-Kun,Jan Shau-Shiun,Hsiao Fei-Bin

Publisher

Springer Science and Business Media LLC

Subject

General Earth and Planetary Sciences

Link

http://link.springer.com/content/pdf/10.1007/s10291-008-0114-z.pdf

Reference19 articles.

1. Axelrad P, Behre CP (1999) Satellite attitude determination based on GPS signal-to-noise ratio. Proc IEEE 87(1):133–144

2. Brown AK (2005) GPS/INS uses low-cost MEMS IMU. IEEE A E Syst Mag:3–10

3. Cho A, Kim J, Lee S et al. (2007) Fully automatic taxiing, takeoff and landing of a UAV only with a single-antenna GPS receiver. In: AIAA Infotech at Aerospace 2007 Conference and Exhibit

4. Chu QP, van Woerkom PTLM (1997) GPS for low-cost attitude determination a review of concept, in-flight experiences, and current developments. Acta Astronaut 41(4):421–433

5. Cohen CE, McNally BD, Parkinson BW (1994) Flight tests of attitude determination using GPS compared against an inertial navigation unit. Navigation 41:83–97

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