Stabilization of spacecraft flight in halo orbits: An H∞ approach

Jayant E. Kulkarni; Mark E. Campbell; Geir E. Dullerud

doi:10.1109/TCST.2006.872517

Stabilization of spacecraft flight in halo orbits: An H_∞ approach

Jayant E. Kulkarni
, Mark E. Campbell
, Geir E. Dullerud

Research output: Contribution to journal › Article › peer-review

58 Scopus citations

Abstract

The problem of stabilizing the motion of a spacecraft in an unstable orbit around the interior Sun-Earth libration point (L₁) is addressed in this paper. Modern control techniques, which extend the traditional H_∞ framework to periodic discrete linear time-varying systems, are employed in the solution of the problem. Nonlinear simulation results are presented and it is shown that the control effort required can be provided by next-generation electric propulsion systems.

Original language	English (US)
Pages (from-to)	572-578
Number of pages	7
Journal	IEEE Transactions on Control Systems Technology
Volume	14
Issue number	3
DOIs	https://doi.org/10.1109/TCST.2006.872517
State	Published - May 2006
Externally published	Yes

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

H optimal control
Halo orbits
Periodic linear time-varying systems

Publisher link

10.1109/TCST.2006.872517

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Cite this

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abstract = "The problem of stabilizing the motion of a spacecraft in an unstable orbit around the interior Sun-Earth libration point (L1) is addressed in this paper. Modern control techniques, which extend the traditional H∞ framework to periodic discrete linear time-varying systems, are employed in the solution of the problem. Nonlinear simulation results are presented and it is shown that the control effort required can be provided by next-generation electric propulsion systems.",

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KW - Halo orbits

KW - Periodic linear time-varying systems

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