Inertial navigation system aided by aircraft dynamics

IEEE Transactions on Control Systems Technology

Volumn 7, Issue 4, 1999, Pages 487-493

  Koifman, M ^a   Bar Itzhack, I Y ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

CONTACT ANGLE; ERROR ANALYSIS; INERTIAL NAVIGATION SYSTEMS; KALMAN FILTERING; MATHEMATICAL MODELS; MATHEMATICAL TRANSFORMATIONS; MATRIX ALGEBRA; OBSERVABILITY; PERTURBATION TECHNIQUES; ROBUSTNESS (CONTROL SYSTEMS); SENSITIVITY ANALYSIS; VECTORS;

CALIBRATION MODELS; LOW GRADE INERTIAL NAVIGATION SYSTEM; TRANSFORMATION MATRIX;

AERODYNAMICS;

EID: 0033165136     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.772164     Document Type: Article

References (5)

1. A. E. Bryson, Jr., "Kalman filter divergence and aircraft motion estimators," J. Guidance Contr., vol. 1, no. 1, pp. 71-78, 1978.
2. M. Sri-Jayantha and R. F. Stengel, "Determination of nonlinear aerodynamic coefficients using the estimation-before-modeling method," J. Aircraft, vol. 25, no. 9, pp. 796-804, 1988.
3. A. J. Grunwald, E. Wahnon, and S. J. Merhav, "Estimation of vehicle attitude and flight-path angles from low cost rate gyro measurements," in Proc. 25th Israel Annu. Conf. Aviation Astronautics, Technion, Haifa, Israel, Feb. 1983, pp. 121-127.
4. M. Koifman and S. J. Merhav, "Autonomously aided strapdown attitude reference system," J. Guidance, Contr, Dynamics, vol. 14, no. 6, pp. 1164-1172, 1991.
5. R. A. Nash, Jr., J. A. D'Appolito, and K. J. Roy, "Error analysis of hybrid aircraft inertial navigation systems," in AIAA Guidance Navigation Contr. Conf., Aug. 1972, AIAA Paper 72-848.