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Event-triggered adaptive attitude control for flexible spacecraft with actuator nonlinearity

  • Published:2020-11 Issue: Volume:106 Page:106111
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Liu Qiuhong,Liu Ming,Shi Yan,Yu Jinyong

Funder

National Natural Science Foundation of China

National Key Research and Development Plan

National Defense Basic Research Program

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Dynamics and control of spacecraft with a large misaligned rotational component;Wu;Aerosp. Sci. Technol.,2019

2. Attitude and vibration control of flexible spacecraft using singular perturbation approach;Shahravi;Int. Sch. Res. Not. Aerosp. Eng.,2014

3. Finite-time fuzzy sampled-data control for nonlinear flexible spacecraft with stochastic actuator failures;Sun;IEEE Trans. Ind. Electron.,2017

4. Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous;Zhang;Aerosp. Sci. Technol.,2020

5. Continuous finite-time extended state observer based fault tolerant control for attitude stabilization;Li;Aerosp. Sci. Technol.,2019

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