ScholarLens Back to search
2012•International Journal of Aeronautical and Space SciencesOpen access

Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area

Sang-Cherl Lee, Hae‐Dong Kim, Jinyoung Suk

Open full text 22 citations

Abstract

In this paper, a collision avoidance maneuver was sought for low Earth orbit (LEO) and geostationary Earth orbit (GEO) satellites maintained in a keeping area. A genetic algorithm was used to obtain both the maneuver start time and the delta-V to reduce the probability of collision with uncontrolled space objects or debris. Numerical simulations demonstrated the feasibility of the proposed algorithm for both LEO satellites and GEO satellites.

Open-access reader

About this research paper

What this paper is about

In this paper, a collision avoidance maneuver was sought for low Earth orbit (LEO) and geostationary Earth orbit (GEO) satellites maintained in a keeping area. A genetic algorithm was used to obtain both the maneuver start time and the delta-V to reduce the probability of collision with uncontrolled space objects or debris. Numerical simulations demonstrated the feasibility of the proposed algorithm for both LEO satellites and GEO satellites.

Why it matters

OpenAlex reports 22 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

In this paper, a collision avoidance maneuver was sought for low Earth orbit (LEO) and geostationary Earth orbit (GEO) satellites maintained in a keeping area. A genetic algorithm was used to obtain both the maneuver start time and the delta-V to reduce the probability of collision with uncontrolled space objects or debris. Numerical simulations demonstrated the feasibility of the proposed algorithm for both LEO satellites and GEO satellites.

Key concepts: Geostationary orbit, Low earth orbit, Collision avoidance, Satellite, Space debris, Medium Earth orbit, Collision, Orbit (dynamics)

Related papers

Related paper 1Related paper 2
Back to paper searchBrowse research topicsOriginal source
Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area — Research Paper | ScholarLens