Fault-tolerant model predictive sliding mode control with fixed-time attitude stabilization and vibration suppression of flexible spacecraft-Reference-Cited by-同舟云学术

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Fault-tolerant model predictive sliding mode control with fixed-time attitude stabilization and vibration suppression of flexible spacecraft

Published:2023-08 Issue: Volume:139 Page:108381
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Khodaverdian Maria,Malekzadeh Maryam^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Finite-time attitude maneuvering and vibration suppression of flexible spacecraft;Zhang;J. Franklin Inst.,2020

2. Robust finite-time control for flexible spacecraft attitude maneuver;Wu;J. Aerosp. Eng.,2014

3. Adaptive fast nonsingular terminal sliding mode control for attitude tracking of flexible spacecraft with rotating appendage;Miao;Aerosp. Sci. Technol.,2019

4. Adaptive quantized sliding mode attitude tracking control for flexible spacecraft with input dead-zone via Takagi-Sugeno fuzzy approach;Li;Inf. Sci.,2022

5. Robust neural-network-based quasi-sliding-mode control for spacecraft-attitude maneuvering with prescribed performance;Fu;Aerosp. Sci. Technol.,2021

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2. An active-passive integrated actuator based on macro fiber composite for on-orbit micro-vibration isolation;Aerospace Science and Technology;2024-11

3. Adaptive fault-tolerant control for ascent HSV with wing damage and function constraints on states;Acta Astronautica;2024-09

4. Prescribed modal vibration control and disturbance load analysis of rigid-flexible satellites;Advances in Space Research;2024-08

5. Improving Terrain Adaptability and Compliance in Closed-Chain Leg: Design, Control, and Testing;Journal of Mechanisms and Robotics;2024-07-19

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