Analysis of star tracker/accelerometer inertial navigation system in theory
Yingbo Cai, Qiuying Wang, Xuetong Wei, LI De-biao · 2011
In the star tracker/accelerometer inertial navigation system, the star tracker will be used to calculate the attitude matrix. The accelerometer is analyzed and integral utilizing the attitude matrix, to get the velocities and position of carrier, the feedback is formative. After star tracker/accelerometer inertial navigation system in theory is resolved, the errors will be discussed and the result will be proved by the simulation test.