Skip to main navigation Skip to search Skip to main content

Switch-based adaptive nonsingular sliding mode control for spacecraft formation flying

  • Ting Wang
  • , Yueyong Lv
  • , Shengliang Zhou
  • , Dongyu Li
  • Harbin Institute of Technology
  • Shanghai Institute of Spaceflight Control Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper investigates the relative position control problem for a two-agent spacecraft formation. The modified nonlinear dynamic based on C-W equation is adopted to describe relative position between the leader and follower. Considering the system uncertainty and external disturbance, adaptive sliding mode control laws based on linear and terminal sliding surface are proposed respectively. In addition, a switching mechanism is employed to make a selection between the general and terminal surfaces so as to avoid singularity. The convergence of closed-loop system is proved by Lyapunov stability theory. Numerical simulations illustrates the validity of the control law proposed.

Original languageEnglish
Title of host publicationProceedings of 2016 2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages195-200
Number of pages6
ISBN (Electronic)9781467398725
DOIs
StatePublished - 14 Dec 2016
Externally publishedYes
Event2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016 - Singapore, Singapore
Duration: 27 Jul 201629 Jul 2016

Publication series

NameProceedings of 2016 2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016

Conference

Conference2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016
Country/TerritorySingapore
CitySingapore
Period27/07/1629/07/16

Keywords

  • Adaptive
  • Nonsigular sliding mode
  • Spacecraft formation flying
  • Switch

Fingerprint

Dive into the research topics of 'Switch-based adaptive nonsingular sliding mode control for spacecraft formation flying'. Together they form a unique fingerprint.

Cite this