Backstepping sliding mode control for mars entry with finite time convergence

Ganghui Shen, Yuanqing Xia*, Dailiang Ma, Jinhui Zhang

*Corresponding author for this work

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

3 Citations (Scopus)

Abstract

There are usually large uncertainties in the aerodynamic parameters of Mars entry vehicles, which inevitably degrades the performance of entry guidance algorithms. The paper presents a backstepping sliding mode controller for drag tracking in Mars entry guidance, which can guarantee the tracking error with finite-time convergence. First, the drag can track the reference trajectory under the virtual control law by introducing a sliding manifold, and the extended state observer (ESO) is used to estimate and counteract the uncertainties. Then, the finite-time convergence of drag tracking error can be achieved under the proposed backstepping sliding mode guidance law. In addition, the rigorous proof of tracking error convergence is given. Finally, numerical simulation results are presented to demonstrate the effectiveness of the proposed guidance law.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages6102-6107
Number of pages6
ISBN (Electronic)9789881563934
DOIs
Publication statusPublished - 7 Sept 2017
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

NameChinese Control Conference, CCC
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • Backstepping
  • Finite time
  • Mars entry
  • Sliding mode control

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