메뉴 건너뛰기




Volumn 29, Issue 2, 2004, Pages 217-235

Estimation of attitudes from a low-cost miniaturized inertial platform using Kalman filter-based sensor fusion algorithm

Author keywords

Estimation of attitudes; Inertial navigation systems; Kalman Filters low cost sensors; Miniatured inertial platform; Sensor fusion algorithm

Indexed keywords

ALGORITHMS; COMPUTER PROGRAMMING; KALMAN FILTERING; MICROCONTROLLERS; MICROELECTROMECHANICAL DEVICES; MICROSENSORS; REMOTELY OPERATED VEHICLES; SENSOR DATA FUSION;

EID: 2442478646     PISSN: 02562499     EISSN: None     Source Type: Journal    
DOI: 10.1007/bf02703733     Document Type: Article
Times cited : (33)

References (12)
  • 9
    • 84894521939 scopus 로고    scopus 로고
    • Aerodynamic model identification and GNC design for the parafoil-Load System ALEX
    • AIAA-2001-2015
    • Jann T 2001 Aerodynamic model identification and GNC design for the parafoil-Load System ALEX. Proc. of AIAA Aerodynamic Systems Decelerator Conference, AIAA-2001-2015
    • (2001) Proc. of AIAA Aerodynamic Systems Decelerator Conference
    • Jann, T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.