Attitude estimation and control based on modified unscented Kalman filter for gyro-less satellite with faulty sensors-Reference-Cited by-同舟云学术

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Attitude estimation and control based on modified unscented Kalman filter for gyro-less satellite with faulty sensors

Published:2022-02 Issue: Volume:191 Page:134-147
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Pourtakdoust Seid H.^ORCID,Mehrjardi M. Fakhari,Hajkarim M.H.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Adaptive fault-tolerant control of spacecraft attitude dynamics with actuator failures;Han;J. Guid. Control Dynam.,2015

2. Robust attitude tracking control of spacecraft under control input magnitude and rate saturations;Zou;Int. J. Robust Nonlinear Control,2016

3. Coordinative coupled attitude and orbit control for satellite formation with multiple uncertainties and actuator saturation;Fan;Acta Astronaut.,2021

4. Robust control allocation for spacecraft attitude tracking under actuator faults;Shen;IEEE Trans. Control Syst. Technol.,2016

5. Real-time implementation of a parameterized model predictive control for attitude control systems of rigid-flexible satellite;Murilo;Mech. Syst. Signal Process.,2021

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