Nonlinear fractional order proportion-integral-derivative active disturbance rejection control method design for hypersonic vehicle attitude control-Reference-Cited by-同舟云学术

Nonlinear fractional order proportion-integral-derivative active disturbance rejection control method design for hypersonic vehicle attitude control

Published:2015-06 Issue: Volume:111 Page:160-169
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Song Jia,Wang Lun,Cai Guobiao,Qi Xiaoqiang

Funder

National Science Foundation

Aeronautical Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

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5. Stability analysis of a hypersonic vehicle controlled by the characteristic model based adaptive controller;Zhang;Sci. China Inf. Sci.,2012

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