Estimation of errors in inertial navigation systems with GPS measurements

IEEE International Symposium on Industrial Electronics

Volumn 3, Issue , 2001, Pages 1477-1483

  Hong, S ^a   Harashima, F ^a   Kwon, S H ^a   Choi, S B ^a   Lee, M H ^a   Lee, H ^a  

^a Pusan National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL COMPLEXITY; COMPUTER SIMULATION; ERROR ANALYSIS; ESTIMATION; GLOBAL POSITIONING SYSTEM; MATHEMATICAL MODELS; MATRIX ALGEBRA; MEASUREMENT ERRORS; OBSERVABILITY; TIME VARYING SYSTEMS; VECTORS;

COMPUTATIONAL LOAD; MULTIANTENNA MEASUREMENT SYSTEM; UNOBSERVABLE MODE;

INERTIAL NAVIGATION SYSTEMS;

EID: 0034839127     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Attitude determination using GPS
2. Flight tests of attitude determination using GPS compared against an inertial navigation unit
3. Inertially aided GPS based attitude heading reference system (AHRS) for general aviation aircraft
4. A low-cost GPS/inertial attitude heading reference system (AHRS) for general aviation applications
5. Nonlinear observer design for integration of DGPS and INS
6. Control theoretic approach to inertial navigation systems
7. Error estimation of INS ground alignment through observability analysis
8. Observability analysis of piece-wise constant systems-Part I: Theory
9. Observability analysis of piece-wise constant systems-Part II: Application to inertial navigation in-flight alignment
10. Observability, eigenvalues, and Kalman filtering
11. A strapdawn inertial algorithm using an earth-fixed cartesian frame
12. An optimal ambiguity resolution technique for attitude determination