Reliable spacecraft rendezvous without velocity measurement

Shaoming He*, Defu Lin

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

10 Citations (Scopus)

Abstract

This paper investigates the problem of finite-time velocity-free autonomous rendezvous for spacecraft in the presence of external disturbances during the terminal phase. First of all, to address the problem of lack of relative velocity measurement, a robust observer is proposed to estimate the unknown relative velocity information in a finite time. It is shown that the effect of external disturbances on the estimation precision can be suppressed to a relatively low level. With the reconstructed velocity information, a finite-time output feedback control law is then formulated to stabilize the rendezvous system. Theoretical analysis and rigorous proof show that the relative position and its rate can converge to a small compacted region in finite time. Numerical simulations are performed to evaluate the performance of the proposed approach in the presence of external disturbances and actuator faults.

Original languageEnglish
Pages (from-to)52-60
Number of pages9
JournalActa Astronautica
Volume144
DOIs
Publication statusPublished - Mar 2018

Keywords

  • Actuator faults
  • External disturbances
  • Finite-time convergence
  • Spacecraft rendezvous
  • Velocity-free

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