Generalized Guidance Scheme for Low-Thrust Orbit Transfer
Joint Authors
Kim, Donghoon
Leeghim, Henzeh
Cho, Dong-Hyun
Jo, Su-Jang
Source
Mathematical Problems in Engineering
Issue
Vol. 2014, Issue 2014 (31 Dec. 2014), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2014-09-15
Country of Publication
Egypt
No. of Pages
9
Main Subjects
Abstract EN
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 withoutany 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 passingthe earth’s shadow area.
American Psychological Association (APA)
Leeghim, Henzeh& Cho, Dong-Hyun& Jo, Su-Jang& Kim, Donghoon. 2014. Generalized Guidance Scheme for Low-Thrust Orbit Transfer. Mathematical Problems in Engineering،Vol. 2014, no. 2014, pp.1-9.
https://search.emarefa.net/detail/BIM-1044246
Modern Language Association (MLA)
Leeghim, Henzeh…[et al.]. Generalized Guidance Scheme for Low-Thrust Orbit Transfer. Mathematical Problems in Engineering No. 2014 (2014), pp.1-9.
https://search.emarefa.net/detail/BIM-1044246
American Medical Association (AMA)
Leeghim, Henzeh& Cho, Dong-Hyun& Jo, Su-Jang& Kim, Donghoon. Generalized Guidance Scheme for Low-Thrust Orbit Transfer. Mathematical Problems in Engineering. 2014. Vol. 2014, no. 2014, pp.1-9.
https://search.emarefa.net/detail/BIM-1044246
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1044246