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Volumn 57, Issue 1, 2004, Pages 85-101

Development of an integrated low-cost GPS/rate of gyro system for attitude determination

Author keywords

Attitude determination; GPS; Integrated system; Raye gyro

Indexed keywords

ACCURACY ASSESSMENT; ERROR ANALYSIS; GPS; KALMAN FILTER; NAVIGATION;

EID: 1642331596     PISSN: 03734633     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0373463303002583     Document Type: Article
Times cited : (22)

References (14)
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  • 3
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    • Hayward, R.C., Gebre-Egziabher, D., Schwall, M., Powell, D. and Wilson, J. (1997) Inertially Aided GPS Based Attitude Heading Reference System (AHRS) for General Aviation Aircraft, Proc. of ION GPS97. Kansas City, MO, September. 1997, pp. 289-298.
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  • 6
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    • Low-cost GPS receivers and their feasibility for attitude determination
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    • Hoyle, V., Lachapelle, G., Cannon, M.E. and Wang, C. (2002) Low-Cost GPS Receivers and their Feasibility for Attitude Determination, Proc. of GPS NTM02, The Institute of Navigation, San Diego, CA, pp.226-234.
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  • 8
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  • 12
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.