Two-stage parametric identification procedure to predict satellite orbital motion
نویسندگان
چکیده
<span>The paper presents a new step-by-step procedure for constructing navigation satellite motion model. At the first stage of procedure, parameters radiation pressure model are estimated using maximum likelihood method. The statistic estimator based on continuous-discrete adaptive unscented Kalman filter is proposed solar estimation. Step-by-step scheme filtering algorithm used software development given. second stage, unaccounted perturbations results residual differences measurements. obtained lead to significant improvement prediction quality trajectory.</span>
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ژورنال
عنوان ژورنال: International Journal of Power Electronics and Drive Systems
سال: 2022
ISSN: ['2722-2578', '2722-256X']
DOI: https://doi.org/10.11591/ijece.v12i5.pp5348-5354