Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication
This work addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances and limited data communication. A hysteretic quantizer is employed for data quantization in the controller-actuator channel to decrease the communication rate and prevent the chatteri...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/1911820 |
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| _version_ | 1832565792873381888 |
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| author | Lei Xing Dechao Ran Jian Zhang Li Huang |
| author_facet | Lei Xing Dechao Ran Jian Zhang Li Huang |
| author_sort | Lei Xing |
| collection | DOAJ |
| description | This work addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances and limited data communication. A hysteretic quantizer is employed for data quantization in the controller-actuator channel to decrease the communication rate and prevent the chattering phenomenon caused by the logarithmic quantizer. Combined with the adding one power integrator method and backstepping technique, a new finite-time tracking control strategy with adaptation law is designed to ensure that the closed-loop system is practical finite-time stable, and that the tracking errors of relative position and velocity are bounded within finite-time despite with limited data communication and external disturbances. Finally, an example is shown to validate the effectiveness of the proposed finite-time tracking controller. |
| format | Article |
| id | doaj-art-78d0161473804ebbaa81f8f112a7069f |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2022-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-78d0161473804ebbaa81f8f112a7069f2025-02-03T01:06:35ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/1911820Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data CommunicationLei Xing0Dechao Ran1Jian Zhang2Li Huang3Research Center of Satellite TechnologyNational Innovation Institute of Defense TechnologyShanghai Institute of Satellite EngineeringBeijing Aerospace Automatic Control InstituteThis work addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances and limited data communication. A hysteretic quantizer is employed for data quantization in the controller-actuator channel to decrease the communication rate and prevent the chattering phenomenon caused by the logarithmic quantizer. Combined with the adding one power integrator method and backstepping technique, a new finite-time tracking control strategy with adaptation law is designed to ensure that the closed-loop system is practical finite-time stable, and that the tracking errors of relative position and velocity are bounded within finite-time despite with limited data communication and external disturbances. Finally, an example is shown to validate the effectiveness of the proposed finite-time tracking controller.http://dx.doi.org/10.1155/2022/1911820 |
| spellingShingle | Lei Xing Dechao Ran Jian Zhang Li Huang Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication International Journal of Aerospace Engineering |
| title | Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication |
| title_full | Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication |
| title_fullStr | Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication |
| title_full_unstemmed | Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication |
| title_short | Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication |
| title_sort | finite time orbit control for spacecraft formation with external disturbances and limited data communication |
| url | http://dx.doi.org/10.1155/2022/1911820 |
| work_keys_str_mv | AT leixing finitetimeorbitcontrolforspacecraftformationwithexternaldisturbancesandlimiteddatacommunication AT dechaoran finitetimeorbitcontrolforspacecraftformationwithexternaldisturbancesandlimiteddatacommunication AT jianzhang finitetimeorbitcontrolforspacecraftformationwithexternaldisturbancesandlimiteddatacommunication AT lihuang finitetimeorbitcontrolforspacecraftformationwithexternaldisturbancesandlimiteddatacommunication |