Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft

The Stewart platform, a classical mechanism proposed as the parallel operation apparatus of robots, is widely used for vibration isolation in various fields. In this paper, a design integrating both small attitude control and vibration isolation for high-precision payloads on board satellites is pro...

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Autores principales:	Weichao Chi, He Ma, Caihua Wang, Tianyu Zhao
Formato:	article
Lenguaje:	EN
Publicado:	MDPI AG 2021
Materias:	parallel mechanism active disturbance rejection control vibration isolation attitude maneuver Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/b8c30dc068ff46b6bf11dadc8d6665fb
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spelling	oai:doaj.org-article:b8c30dc068ff46b6bf11dadc8d6665fb2021-11-25T15:57:31ZResearch on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft10.3390/aerospace81103332226-4310https://doaj.org/article/b8c30dc068ff46b6bf11dadc8d6665fb2021-11-01T00:00:00Zhttps://www.mdpi.com/2226-4310/8/11/333https://doaj.org/toc/2226-4310The Stewart platform, a classical mechanism proposed as the parallel operation apparatus of robots, is widely used for vibration isolation in various fields. In this paper, a design integrating both small attitude control and vibration isolation for high-precision payloads on board satellites is proposed. Our design is based on a Stewart platform equipped with voice-coil motors (VCM) to provide control force over the mechanism. The coupling terms in the dynamic equations of the legs are removed as the total disturbance by the linear active disturbance rejection control (LADRC). Attitude maneuver and vibration isolation performance is verified by numerical simulations.Weichao ChiHe MaCaihua WangTianyu ZhaoMDPI AGarticleparallel mechanismactive disturbance rejection controlvibration isolationattitude maneuverMotor vehicles. Aeronautics. AstronauticsTL1-4050ENAerospace, Vol 8, Iss 333, p 333 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	parallel mechanism active disturbance rejection control vibration isolation attitude maneuver Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	parallel mechanism active disturbance rejection control vibration isolation attitude maneuver Motor vehicles. Aeronautics. Astronautics TL1-4050 Weichao Chi He Ma Caihua Wang Tianyu Zhao Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
description	The Stewart platform, a classical mechanism proposed as the parallel operation apparatus of robots, is widely used for vibration isolation in various fields. In this paper, a design integrating both small attitude control and vibration isolation for high-precision payloads on board satellites is proposed. Our design is based on a Stewart platform equipped with voice-coil motors (VCM) to provide control force over the mechanism. The coupling terms in the dynamic equations of the legs are removed as the total disturbance by the linear active disturbance rejection control (LADRC). Attitude maneuver and vibration isolation performance is verified by numerical simulations.
format	article
author	Weichao Chi He Ma Caihua Wang Tianyu Zhao
author_facet	Weichao Chi He Ma Caihua Wang Tianyu Zhao
author_sort	Weichao Chi
title	Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
title_short	Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
title_full	Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
title_fullStr	Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
title_full_unstemmed	Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft
title_sort	research on control of stewart platform integrating small attitude maneuver and vibration isolation for high-precision payloads on spacecraft
publisher	MDPI AG
publishDate	2021
url	https://doaj.org/article/b8c30dc068ff46b6bf11dadc8d6665fb
work_keys_str_mv	AT weichaochi researchoncontrolofstewartplatformintegratingsmallattitudemaneuverandvibrationisolationforhighprecisionpayloadsonspacecraft AT hema researchoncontrolofstewartplatformintegratingsmallattitudemaneuverandvibrationisolationforhighprecisionpayloadsonspacecraft AT caihuawang researchoncontrolofstewartplatformintegratingsmallattitudemaneuverandvibrationisolationforhighprecisionpayloadsonspacecraft AT tianyuzhao researchoncontrolofstewartplatformintegratingsmallattitudemaneuverandvibrationisolationforhighprecisionpayloadsonspacecraft
_version_	1718413402602209280

Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft

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