Navigation sensor, filter, and failure mode simulation results using the distributed Kalman filter simulator (DKFSIM)

Record - IEEE PLANS, Position Location and Navigation Symposium

Volumn , Issue , 1996, Pages 697-710

  Lawrence Jr , Paul J ^a   Berarducci, Michael P ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; COMPUTER HARDWARE; COMPUTER SIMULATION; COMPUTER SOFTWARE; FAILURE ANALYSIS; FORTRAN (PROGRAMMING LANGUAGE); GLOBAL POSITIONING SYSTEM; KALMAN FILTERING; MATHEMATICAL MODELS; RADIO ALTIMETERS; SENSORS; SYNTHETIC APERTURE RADAR;

DISTRIBUTED KALMAN FILTER SIMULATOR; FAILURE MODE SIMULATION; NAVIGATION SENSOR; PRECISION VELOCITY UPDATE MODEL;

INERTIAL NAVIGATION SYSTEMS;

EID: 0029697323     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)