On the observability of loosely coupled global positioning system/inertial navigation system integrations with five degree of freedom and four degree of freedom inertial measurement units

Journal of Dynamic Systems, Measurement and Control, Transactions of the ASME

Volumn 136, Issue 2, 2014, Pages

  Ryan, Jonathan G ^a   Bevly, David M ^b  

^a FREDERICK NATIONAL LABORATORY FOR CANCER RESEARCH   (United States)

^b AUBURN UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE ESTIMATION; COURSE INFORMATION; DEGREE OF FREEDOM; ERROR CHARACTERISTICS; FOUR DEGREE OF FREEDOM; INERTIAL MEASUREMENT UNIT; LOOSELY-COUPLED INTEGRATION; SYSTEM INTEGRATION;

DEGREES OF FREEDOM (MECHANICS); GLOBAL POSITIONING SYSTEM; INTEGRATION; MONTE CARLO METHODS; NAVIGATION SYSTEMS; OBSERVABILITY; TRACKING (POSITION);

UNITS OF MEASUREMENT;

EID: 84892694745     PISSN: 00220434     EISSN: 15289028     Source Type: Journal    
DOI: 10.1115/1.4025985     Document Type: Article

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