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Discrete control method for the formation flying around Lagrange point

  • Sheng Ping Gong*
  • , Jun Feng Li
  • , He Xi Baoyin
  • , Yun Feng Gao
  • *Corresponding author for this work
  • Tsinghua University

Research output: Contribution to journalArticlepeer-review

Abstract

The formation flying around Lagrange points will benefit deep space exploration greatly due to the special location of the Lagrange points. The paper investigated the discrete control method for the formation flying around the Lagrange point. First, a simple iterative algorithm, which could calculate the control quantity, was given. Based on this algorithm, two control strategies were introduced. Then, several performance indexes related to formation error and energy consumption were defined. By simulating the circular formation flying examples, two strategies are compared and analyzed. The simulation results show that strategy two superior to strategy one either in energy consumption or in error control. For strategy two, the energy consumption increases with formation radius when the impulse time span is fixed. When the formation radius is fixed, the formation error decrease with the impulse time span exponentially. But the energy consumption changes slightly with the impulse time span.

Original languageEnglish
Pages (from-to)77-81
Number of pages5
JournalYuhang Xuebao/Journal of Astronautics
Volume28
Issue number1
StatePublished - Jan 2007
Externally publishedYes

UN SDGs

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

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

Keywords

  • Formation flying
  • Impulse control
  • Lagrange point
  • Three body problem

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