About this document
Gimbaled INS Transfer Alignment Model by Gökhan Kiremit is a document available to read on EtoBox.
The document presents a method for attitude matching alignment of gimbaled inertial navigation systems (INS) on a moving base using a Kalman filter to estimate misalignment angles. The proposed model achieves an alignment accuracy of 40 arc seconds within approximately 30 seconds, making it suitable for applications such as warship missile systems. The paper discusses the dynamics of the gimbaled INS, the relationship between fixed and misalignment angles, and provides simulation results to validate the eff
- Author
- Gökhan Kiremit
- Language
- EN