USE OF AN EXTERNAL CASCADED KALMAN FILTER TO IMPROVE THE PERFORMANCE OF A GLOBAL POSITIONING SYSTEM (GPS) INERTIAL NAVIGATOR.

IEEE Proceedings of the National Aerospace and Electronics Conference

Volumn , Issue , 1988, Pages 345-350

  Schlee, F H ^a   Toda, N F ^a   Islam, M A ^a   Standish, C J ^a  

^a IBM   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NAVIGATION - INERTIAL SYSTEMS; RADIO NAVIGATION;

ATTITUDE HEADING REFERENCE SYSTEM (AHRS); EXTERNAL CASCADED KALMAN FILTER; GPS INERTIAL NAVIGATOR; GPS/INS INTEGRATION; IN-AIR INERTIAL NAVIGATION SYSTEM;

SIGNAL FILTERING AND PREDICTION;

EID: 0023779656     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)