Attitude control of spacecraft simulator without angular velocity measurement-Reference-Cited by-同舟云学术

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Attitude control of spacecraft simulator without angular velocity measurement

Published:2019-03 Issue: Volume:84 Page:72-81
ISSN:0967-0661
Container-title:Control Engineering Practice
language:en
Short-container-title:Control Engineering Practice

Author:

Malekzadeh Maryam,Sadeghian Hamid

Funder

Iran National Science FoundationIran National Science Foundation (INSF)

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference32 articles.

1. Adaptive quaternion tracking with nonlinear extended state observer;Bai;Acta Astronautica,2017

2. Conceptual design of a low-cost real-time hardware-in-the-loop simulator for satellite attitude control system;Bayat;Turkish Journal of Electrical Engineering and Computer Science,2015

3. Time efficient spacecraft maneuver using constrained torque distribution;Cao;Acta Astronautica,2016

4. Design, implementation and validation of the kompsat spacecraft simulator;Choi;International Journal of Aeronautical and Space Sciences,2000

5. Emulating scaled clohessy–wiltshire dynamics on an air-bearing spacecraft simulation testbed;Ciarcià;Journal of Guidance, Control and Dynamics,2017

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1. Finite time sliding mode control for agile rigid satellite with CMG actuators using fast high-order sliding mode observer;Aerospace Systems;2024-03-29

2. Automatic Mass Balancing of a Small Spherical Simulator for Attitude Control Verification;IEEE Access;2024

3. Finite-time Observer Based Predefined-time Aircraft Attitude Tracking Control;International Journal of Control, Automation and Systems;2023-09-25

4. Applied nonlinear control of spacecraft simulator with constraints on torque and momentum of reaction wheels;ISA Transactions;2023-07

5. Applied Optimal Control of Spacecraft Simulator Subject to Failures of Reaction Wheels;Arabian Journal for Science and Engineering;2023-06-08

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