Skip to main navigation Skip to search Skip to main content

Fault-tolerant control for carrier rocket actuator based on adaptive control with constraints

  • Beihang University

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

Abstract

A fault-tolerant control (FTC) for carrier rocket with actuator fault using model reference adaptive control (MRAC) method is proposed in this paper. Firstly, the model for the carrier rocket with actuator fault is established by treating the fault as disturbance. Based on the flight dynamic model, the linear quadratic regulator (LQR) technique is used as the basic controller to make the output response follow the command signal. Moreover, in the case of actuator constraints, the fault-tolerant controller is designed using MRAC to minigate the effect of actuator fault with anti-windup compensation. Finally, a numerical example is given to demonstrate the effectiveness of the proposed methods.

Original languageEnglish
Title of host publicationProceedings - 2020 35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages509-514
Number of pages6
ISBN (Electronic)9781728176840
DOIs
StatePublished - 16 Oct 2020
Event35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020 - Zhanjiang, China
Duration: 16 Oct 202018 Oct 2020

Publication series

NameProceedings - 2020 35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020

Conference

Conference35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
Country/TerritoryChina
CityZhanjiang
Period16/10/2018/10/20

Keywords

  • Actuator fault
  • Anti-windup
  • Fault-tolerant control (FTC)
  • Model reference adaptive control (MRAC)

Fingerprint

Dive into the research topics of 'Fault-tolerant control for carrier rocket actuator based on adaptive control with constraints'. Together they form a unique fingerprint.

Cite this