Disturbance observer-based finite-time attitude maneuver control for micro satellite under actuator deviation fault-Reference-Cited by-同舟云学术

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Disturbance observer-based finite-time attitude maneuver control for micro satellite under actuator deviation fault

Published:2018-11 Issue: Volume:82-83 Page:262-271
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Qiao Jianzhong,Zhang Dafa,Zhu Yukai,Zhang Peixi

Funder

National Natural Science Foundation of China

Program for Changjiang Scholars and Innovative Research Team in University

Innovative Research Team of National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Discussions on attitude determination and control system for micro/nano/pico-satellites considering survivability based on Hodoyoshi-3 and 4 experiences;Nakasuka;Acta Astronaut.,2018

2. Compensation of time-variable magnetic moments for a precise attitude control in nano- and micro-satellite missions;Inamori;Adv. Space Res.,2011

3. Development and experimental validation of a multi-algorithmic hybrid attitude determination and control system for a small satellite;Lee;Aerosp. Sci. Technol.,2018

4. Distributed fault-tolerant control design for rigid spacecraft finite-time attitude synchronization;Zhou;Int. J. Robust Nonlinear Control,2016

5. Robust and optimal attitude control of spacecraft with inertia uncertainties using minimal kinematic parameters;Park;Aerosp. Sci. Technol.,2016

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