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vol 63 / July, 2020
Article

DOI 10.17586/0021-3454-2020-63-1-35-45

UDC 523.34:629.78:527.62

METHOD FOR CALCULATING THE ACCURACY CHARACTERISTICS OF AUTONOMOUS SYSTEM OF SPACECRAFT NAVIGATION AND ORIENTATION

V. I. Kuznetsov
A. F. Mozhaysky Military Space Academy, Department 34 of the Military Institute;


Калашников С. Д.
ВКА им. А. Ф. Можайского, Военный институт (научно-исследовательский);


Миклин Д. В.
ВКА им. А. Ф. Можайского, Военный институт (научно-исследовательский);


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Abstract. Results of development of a method for evaluating the accuracy of autonomous system of spacecraft navigation and orientation are presented. Advantages of the autonomous approach and the current state of the theory and practice of modeling the processes of functioning of autonomous spacecraft navigation systems are considered. The proposed method allows to provide a sufficiently high accuracy of ephemerides, which is maintained for a long time. Results of estimation of orbit parameters for various algorithms for solving navigation problems obtained with the use of the developed automated system of scientific research are demonstrated.
Keywords: spacecraft autonomy, spacecraft self-determination, autonomous navigation, autonomous orientation

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