Formation Flying of small Satellites Using Coulomb Force

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The formation flying of satellites has been identified as an enabling technology for many future space missions. The application of conventional thrusters for formation flying usually results in high cost, limited life-time, and a large weight penalty. Various methods including the use of coulomb forces have been considered as an alternative to the conventional thrusters. In the present investigation, we investigate the feasibility of achieving the desired formation using Coulomb forces. This method has several advantages including low cost, light weight and no contamination. A simple controller based on the relative position and velocity errors between the leader and follower satellites is developed. The proposed controller is applied to circular formations considering the effects of disturbances in initial formation conditions as well as system nonlinearity. Results of the numerical simulation state that the proposed controller is successful in establishing circular formations of leader and follower satellites, for a formation size below 100 m.
Publisher
The Korean Society for Aeronautical & Space Sciences
Issue Date
2006-05
Keywords

Formation flying; Coulomb forece; Lyapunov stability

Citation

KSAS International Journal, Vol.7, No.1, pp.84-90

URI
http://hdl.handle.net/10203/15261
Link
http://www.ksas.or.kr/
Appears in Collection
AE-Journal Papers(저널논문)

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