Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion

Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion

In this article, the spacecraft attitude takeover control (ATC) problem with limited communication and the unavailable angular velocity using cellular satellites is addressed. First, a dynamic uniform quantizer (DUQ) is proposed to quantize unit quaternion between sensor cellular satellites and cont...

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Main Authors: Ning, Kai, Wu, Baolin, Wang, Danwei
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2023
Subjects:
Engineering::Electrical and electronic engineering
Attitude Takeover Control
Cellular Satellite
Online Access:https://hdl.handle.net/10356/170681
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1706812023-09-26T01:12:30Z Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion Ning, Kai Wu, Baolin Wang, Danwei School of Electrical and Electronic Engineering Engineering::Electrical and electronic engineering Attitude Takeover Control Cellular Satellite In this article, the spacecraft attitude takeover control (ATC) problem with limited communication and the unavailable angular velocity using cellular satellites is addressed. First, a dynamic uniform quantizer (DUQ) is proposed to quantize unit quaternion between sensor cellular satellites and controller cellular satellite. Second, an adaptive fuzzy observer is proposed to estimate the unavailable angular velocity. Further, between controller cellular satellite and actuator cellular satellites, an event-triggered mechanism (ETM) is provided to lighten the communication burden. By combing DUQ, adaptive fuzzy observer, the adaptive fuzzy control law and the ETM is established. The stability of the ATC systems with the proposed control method is ensured. Finally, the simulation results illustrate the effectiveness of the developed control laws. This work was supported by the National Natural Science Foundation of China under Grant 61873312. 2023-09-26T01:12:30Z 2023-09-26T01:12:30Z 2023 Journal Article Ning, K., Wu, B. & Wang, D. (2023). Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion. IEEE Transactions On Aerospace and Electronic Systems, 59(4), 4168-4179. https://dx.doi.org/10.1109/TAES.2023.3237127 0018-9251 https://hdl.handle.net/10356/170681 10.1109/TAES.2023.3237127 2-s2.0-85147270894 4 59 4168 4179 en IEEE Transactions on Aerospace and Electronic Systems © 2023 IEEE. All rights reserved.
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Electrical and electronic engineering
Attitude Takeover Control
Cellular Satellite
spellingShingle Engineering::Electrical and electronic engineering
Attitude Takeover Control
Cellular Satellite
Ning, Kai
Wu, Baolin
Wang, Danwei
Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
description In this article, the spacecraft attitude takeover control (ATC) problem with limited communication and the unavailable angular velocity using cellular satellites is addressed. First, a dynamic uniform quantizer (DUQ) is proposed to quantize unit quaternion between sensor cellular satellites and controller cellular satellite. Second, an adaptive fuzzy observer is proposed to estimate the unavailable angular velocity. Further, between controller cellular satellite and actuator cellular satellites, an event-triggered mechanism (ETM) is provided to lighten the communication burden. By combing DUQ, adaptive fuzzy observer, the adaptive fuzzy control law and the ETM is established. The stability of the ATC systems with the proposed control method is ensured. Finally, the simulation results illustrate the effectiveness of the developed control laws.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Ning, Kai
Wu, Baolin
Wang, Danwei
format Article
author Ning, Kai
Wu, Baolin
Wang, Danwei
author_sort Ning, Kai
title Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
title_short Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
title_full Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
title_fullStr Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
title_full_unstemmed Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
title_sort velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
publishDate 2023
url https://hdl.handle.net/10356/170681
_version_ 1779156741453250560

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