A SDINS Compensation Scheme Using Electro-Optical Sensor

This paper presents a navigation error compensation scheme for Strap-Down Inertial Navigation System(SDINS) using electro-optical sensor. The proposed scheme uses the position or the attitude information from the sensor. For each case, Kalman filter model is derived and implemented. To show the effectiveness of the present compensation scheme, computer simulations have been carried out resulting in the boundedness of position and attitude errors.

[1]  A. Wu SBIRS high payload LOS attitude determination and calibration , 1998, 1998 IEEE Aerospace Conference Proceedings (Cat. No.98TH8339).

[2]  M. S. Grewal,et al.  Application of Kalman filtering to the calibration and alignment of inertial navigation systems , 1990, 29th IEEE Conference on Decision and Control.