Sliding mode control for decentralized spacecraft formation flying using geometric mechanics

Daero Lee, Eric Butcher, Amit K. Sanyal

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper presents a sliding mode control-based tracking control scheme for decentralized spacecraft formation flying via a virtual leader state trajectory. The configuration space for a spacecraft is the Lie group SE(3), which is the set of positions and orientations of the rigid spacecraft in three-dimensional Euclidean space. A virtual leader trajectory, in the form of natural attitude and translational (orbital) motion of a satellite, is generated off-line. Each spacecraft tracks a desired relative configuration with respect to the virtual leader in a decentralized and autonomous manner, to achieve the desired formation. The relative configuration between a spacecraft and the virtual leader is described in terms of exponential coordinates on SE(3). A sliding surface is defined using the exponential coordinates and velocity tracking errors. A Lyapunov analysis guarantees that the spacecraft asymptotically converge to their desired state. This tracking control scheme is combined with a collision avoidance input generated from artificial potentials for each spacecraft, which includes information of relative positions of other spacecraft within communications range. Asymptotic convergence to the desired trajectory with this combined control law is demonstrated using a Lyapunov analysis. Numerical simulations are performed to demonstrate the successful application of this tracking control scheme for a decentralized formation maneuver with collision avoidance in the presence of model uncertainty and unknown external disturbances.

Original languageEnglish (US)
Title of host publicationAdvances in the Astronautical Sciences
PublisherUnivelt Inc.
Pages3149-3168
Number of pages20
Volume150
ISBN (Print)9780877036050
Publication statusPublished - 2014
Externally publishedYes
Event2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013 - Hilton Head Island, SC, United States
Duration: Aug 11 2013Aug 15 2013

Other

Other2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013
CountryUnited States
CityHilton Head Island, SC
Period8/11/138/15/13

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ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Lee, D., Butcher, E., & Sanyal, A. K. (2014). Sliding mode control for decentralized spacecraft formation flying using geometric mechanics. In Advances in the Astronautical Sciences (Vol. 150, pp. 3149-3168). Univelt Inc..