Image navigation and registration accuracy improvement using parametric systematic error correction
a system of error correction and image navigation technology, applied in the field of global observation methods and systems, can solve the problems of coarse attitude accuracy, requiring greater accuracy, and costing the equipment of the star tracker to detect faint star light and maintain the star tabl
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[0057]In FIG. 1 there is depicted a block diagram of the method and system of the instant invention. Therein there is seen the ParSEC iteration process of the instant invention wherein coordinate data for stars (Eo, No), visible and IR landmarks (Eo, No) and range are transmitted to an orbit and attitude determination system (OADS) (10). The OADS output is directed to an orbit and attitude solution (O&A) (90) and (100) which contains the iteration measurement residuals Ei-1−Ep.i-1, Np.i-1−Np.i-1 relating to stars (E0, No), and visible and IR landmarks (Eo, No) to be processed by the ParSEC (Ei, Ni) vs. (Ei-1, Ni-1) coefficient determination algorithm (140) of the instant invention. The ParSEC coefficients are thus generated (150) representing the ith ParSEC iteration which is inputted to the ParSEC EiNi vs. Eo, No coefficient determination algorithm (160). The output from (160) is then inputted as the i-1 iteration ParSEC solution (80) to the OADS (10) to improve the O&A solution (9...
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