Generalized Guidance Scheme for Low-Thrust Orbit Transfer

Author:

Leeghim Henzeh1,Cho Dong-Hyun2,Jo Su-Jang3,Kim Donghoon4ORCID

Affiliation:

1. Department of Aerospace Engineering, Chosun University, Gwangju 501-759, Republic of Korea

2. Future Convergence Research Division, Korea Aerospace Research Institute, Daejeon 305-806, Republic of Korea

3. Department of Aerospace Engineering, KAIST, Daejeon 305-701, Republic of Korea

4. Texas A&M University, College Station, TX 77843-3141, USA

Abstract

The authors present an orbital guidance scheme for the satellite with an electrical propulsion system using a Lyapunov feedback control. The construction of a Lyapunov candidate is based on orbital elements, which consist of angular momentum and eccentricity vectors. This approach performs orbit transfers between any two arbitrary elliptic or circular orbits without any singularity issues. These orbital elements uniquely describe a non degenerate Keplerian orbit. The authors improve the reliability of the existing Lyapunov orbital guidance scheme by considering the energy term. Additional improvement is achieved by adding the penalty function. Furthermore, it is shown that the final suggested approach is suitable for the satellite passing the earth’s shadow area.

Funder

Korea Research Council of Fundamental Science and Technology

Publisher

Hindawi Limited

Subject

General Engineering,General Mathematics

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