Ballistic aspects of large-size space debris flyby at low Earth near-circular orbits

The paper is concerned with groups of large-size space debris at low Earth near-circular orbits, which were classified from the analysis of the catalog of space objects. An estimation of the summary characteristic velocity required for a flyby of the three highlighted groups is derived. In this prob...

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Veröffentlicht in:Journal of computer & systems sciences international 2015-07, Vol.54 (4), p.639-650
Hauptverfasser: Baranov, A. A., Grishko, D. A.
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description The paper is concerned with groups of large-size space debris at low Earth near-circular orbits, which were classified from the analysis of the catalog of space objects. An estimation of the summary characteristic velocity required for a flyby of the three highlighted groups is derived. In this problem, a method of reducing the energetic and temporal costs is proposed, which is capable of optimizing the flyby plan of objects of the group. Examples of the summary characteristic velocity calculation are given that is necessary for a flyby of the elements of a group with a flexible choice of flight duration between two neighboring objects. It is shown that a flyby of all the objects of a group of large-size space debris cannot be achieved using a single modern space vehicle.
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subjects Altitude
Analysis
Control
Control Systems of Moving Objects
Earth
Engineering
Mathematical analysis
Mechatronics
Optimization
Orbits
Robotics
Space debris
Space vehicles
Studies
Summaries
Temporal logic
Tracking control systems
Velocity
title Ballistic aspects of large-size space debris flyby at low Earth near-circular orbits
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