DOI 10.17586/0021-3454-2025-68-4-296-302
UDC 629.78
ALGORITHM FOR TERMINAL CONTROL OF A SPACE ROBOT APPROACH TO AN ORBITING OBJECT
A. F. Mozhaisky Military Space Academy, Department of Autonomous Control Systems;
D. E. Polyakov
A. F. Mozhaisky Military Space Academy, Department of Autonomous Control Systems ;
Reference for citation: Ananenko V. M., Polyakov D. E.Algorithm for terminal control of a space robot approach to an orbiting object. Journal of Instrument Engineering. 2025. Vol. 68, N 4. P. 296–302 (in Russian). DOI: 10.17586/0021-3454-2025-68-4-296-302.
Abstract. An algorithm for terminal control of the approach of a space robot to an orbital object located in a coplanar orbit is proposed. The range, relative approach velocity, and angular velocity of the line of sight are selected as input parameters of the algorithm. The results of numerical modeling of the approach process of a space robot to an orbital object, performed according to the proposed algorithm, are presented.
Abstract. An algorithm for terminal control of the approach of a space robot to an orbital object located in a coplanar orbit is proposed. The range, relative approach velocity, and angular velocity of the line of sight are selected as input parameters of the algorithm. The results of numerical modeling of the approach process of a space robot to an orbital object, performed according to the proposed algorithm, are presented.
Keywords: terminal control, space robot, approach, orbital object
References:
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