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http://dx.doi.org/10.5139/JKSAS.2018.46.11.902

Spacecraft Intercept on Non-coplanar Elliptical Orbit Considering J2 Perturbation  

Oghim, Snyoll (Dept. of Aerospace Engineering, Chosun University)
Leeghim, Henzeh (Dept. of Aerospace Engineering, Chosun University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.46, no.11, 2018 , pp. 902-910 More about this Journal
Abstract
This paper deals with spacecraft intercept problem on non-coplanar elliptical obit considering J2 perturbation. This disturbance addressed in this work is a major factor changing the trajectory of a spacecraft orbiting the Earth. To resolve this issue, a real-time intercept method is proposed. This method is based on the optimization problem which consist of the equation of motion considering spherical earth and impulse, and the optimal solution numerically obtained is set as the direction of the thrust of the interceptor. The position error is resolved by iteratively solving the optimization problem and modifying the direction of thrust of interceptor. The proposed method in this paper is verified by using various numerical examples.
Keywords
Spacecraft Intercept; Perturbation; Thrust; Real-Time; Non-coplanar; Elliptic orbit;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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