PD-like finite time controller with simple structure for satellite attitude control-Reference-Cited by-同舟云学术

PD-like finite time controller with simple structure for satellite attitude control

Published:2022-06 Issue: Volume: Page:
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

You Li,Dong Ye,Bing Xiao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference34 articles.

1. Field-of-view limited guidance with impact angle constraint and feasibility analysis;Hu;Aero Sci Technol,2021

2. Incremental twisting fault tolerant control for hypersonic vehicles with partial model knowledge;Han;IEEE Trans Ind Inf,2022

3. Nonlinear optimal attitude control of spacecraft using novel state-dependent coefficient parameterizations;Yao;Aero Sci Technol,2021

4. Time efficient robust PID plus controller for satellite attitude stabilization control considering angular velocity and control torque constraint;Li;J Aero Eng,2017

5. A constrained optimal PID-like controller design for spacecraft attitude stabilization;Li;Acta Astronaut,2012

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