Design of missile autopilot with aerodynamic lift and reaction jets based on auto disturbance rejection controller

Chong Yang, Zhang Ke, Lu Mei Bai

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

1 Scopus citations

Abstract

First a new autopilot design model is presented for the interceptor missile with the blended aerodynamic lift and reaction jet. The reaction jet can improve the response speed, but the structure of control system becomes more complex. Therefore how to design control strategy properly is an urgent problem. Second, considering the discrete property of the lateral pulse jet thrusters and the continuous property of the aerodynamic fins, a kind of ADRC (active disturbance rejection control) autopilot system was designed for the aerodynamic lift/reaction jet missile. Finally, through a testing in the simulation of MATLAB, it is shown that, due to the sufficient utilization of the reaction jet, there is a significant improvement in the fast response and robust performance of the proposed controller. It is applicable to design the autopilot of aerodynamic lift and reaction jet blended missile.

Original languageEnglish
Title of host publicationAdvanced Manufacturing Technology
PublisherTrans Tech Publications Ltd
Pages1036-1039
Number of pages4
ISBN (Print)9783037853702
DOIs
StatePublished - 2012
Event3rd international Conference on Manufacturing Science and Engineering, ICMSE 2012 - Xiamen, China
Duration: 27 Mar 201229 Mar 2012

Publication series

NameAdvanced Materials Research
Volume472-475
ISSN (Print)1022-6680

Conference

Conference3rd international Conference on Manufacturing Science and Engineering, ICMSE 2012
Country/TerritoryChina
CityXiamen
Period27/03/1229/03/12

Keywords

  • Aerodynamic lift and reaction jet
  • Auto disturbance rejection controller
  • Compound control

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