The invention relates to a high-precision
star sensor installation matrix in-
orbit real-time calibration method. The method comprises the steps that actual measurement installation relation
quaternion is resolved, the vector part of the installation relation
quaternion is subjected to filtering and calibration, and an installation matrix is resolved by means of the calibrated installation relation
quaternion. Accordingly, on the condition that no accurate
prior information exists, filter is given by measuring a residual sequence to achieve criterion convergence, if convergence is conducted, a
decay factor takes 1, and a parameter R is estimated online so as to avoid criterion convergence failure; if
divergence is conducted, the
decay factor is resolved in real time, the weight of current beat in the filtering process is adjusted, and the problem that due to the fact that a model is inaccurate, the filer performance is lowered or even
divergence is conducted can be effectively solved. Accordingly, real-time caliberation compensation is conducted on the installation matrix, a large amount of measurement information does not need to be stored, the vector of the installation relation quaternion is filtered directly, but not a three-axis euler angle, and an error introduced by reverse triangle resolving is avoided.