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Algorithm for Terminal Control of a Space Robot Approach to an Orbiting Object

https://doi.org/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.

About the Authors

V. M. Ananenko
A. F. Mozhaisky Military Space Academy
Russian Federation

Vladimir M. Ananenko — PhD, Associate Professor; Senior lecturer

St. Petersburg



D. E. Polyakov
A. F. Mozhaisky Military Space Academy
Russian Federation

Dmitry E. Polyakov — Military student; Department of Autonomous Control Systems

St. Petersburg



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Review

For citations:


Ananenko V.M., Polyakov D.E. Algorithm for Terminal Control of a Space Robot Approach to an Orbiting Object. Journal of Instrument Engineering. 2025;68(4):296-302. (In Russ.) https://doi.org/10.17586/0021-3454-2025-68-4-296-302

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ISSN 0021-3454 (Print)
ISSN 2500-0381 (Online)