Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference
This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication sch...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
LI, Peiran [verfasserIn] WEN, Xin [verfasserIn] LIU, Haiying [verfasserIn] LU, Yuping [verfasserIn] |
|---|
| Format: |
E-Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
2022 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Chinese journal of aeronautics - Amsterdam [u.a.] : Elsevier, 2002, 36, Seite 241-255 |
|---|---|
| Übergeordnetes Werk: |
volume:36 ; pages:241-255 |
| DOI / URN: |
10.1016/j.cja.2022.08.014 |
|---|
| Katalog-ID: |
ELV008998914 |
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| 245 | 1 | 0 | |a Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference |
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| 520 | |a This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. | ||
| 650 | 4 | |a Attitude control | |
| 650 | 4 | |a Cooperative communication | |
| 650 | 4 | |a Discrete time control systems | |
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| 650 | 4 | |a Spacecraft | |
| 700 | 1 | |a WEN, Xin |e verfasserin |4 aut | |
| 700 | 1 | |a LIU, Haiying |e verfasserin |4 aut | |
| 700 | 1 | |a LU, Yuping |e verfasserin |4 aut | |
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10.1016/j.cja.2022.08.014 doi (DE-627)ELV008998914 (ELSEVIER)S1000-9361(22)00184-4 DE-627 ger DE-627 rda eng 380 DE-600 6,25 ssgn ASIEN DE-1a fid LI, Peiran verfasserin aut Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft WEN, Xin verfasserin aut LIU, Haiying verfasserin aut LU, Yuping verfasserin aut Enthalten in Chinese journal of aeronautics Amsterdam [u.a.] : Elsevier, 2002 36, Seite 241-255 Online-Ressource (DE-627)534059384 (DE-600)2365081-3 (DE-576)267763506 1000-9361 nnns volume:36 pages:241-255 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2004 GBV_ILN_2014 GBV_ILN_2068 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 36 241-255 |
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10.1016/j.cja.2022.08.014 doi (DE-627)ELV008998914 (ELSEVIER)S1000-9361(22)00184-4 DE-627 ger DE-627 rda eng 380 DE-600 6,25 ssgn ASIEN DE-1a fid LI, Peiran verfasserin aut Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft WEN, Xin verfasserin aut LIU, Haiying verfasserin aut LU, Yuping verfasserin aut Enthalten in Chinese journal of aeronautics Amsterdam [u.a.] : Elsevier, 2002 36, Seite 241-255 Online-Ressource (DE-627)534059384 (DE-600)2365081-3 (DE-576)267763506 1000-9361 nnns volume:36 pages:241-255 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2004 GBV_ILN_2014 GBV_ILN_2068 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 36 241-255 |
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10.1016/j.cja.2022.08.014 doi (DE-627)ELV008998914 (ELSEVIER)S1000-9361(22)00184-4 DE-627 ger DE-627 rda eng 380 DE-600 6,25 ssgn ASIEN DE-1a fid LI, Peiran verfasserin aut Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft WEN, Xin verfasserin aut LIU, Haiying verfasserin aut LU, Yuping verfasserin aut Enthalten in Chinese journal of aeronautics Amsterdam [u.a.] : Elsevier, 2002 36, Seite 241-255 Online-Ressource (DE-627)534059384 (DE-600)2365081-3 (DE-576)267763506 1000-9361 nnns volume:36 pages:241-255 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2004 GBV_ILN_2014 GBV_ILN_2068 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 36 241-255 |
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10.1016/j.cja.2022.08.014 doi (DE-627)ELV008998914 (ELSEVIER)S1000-9361(22)00184-4 DE-627 ger DE-627 rda eng 380 DE-600 6,25 ssgn ASIEN DE-1a fid LI, Peiran verfasserin aut Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft WEN, Xin verfasserin aut LIU, Haiying verfasserin aut LU, Yuping verfasserin aut Enthalten in Chinese journal of aeronautics Amsterdam [u.a.] : Elsevier, 2002 36, Seite 241-255 Online-Ressource (DE-627)534059384 (DE-600)2365081-3 (DE-576)267763506 1000-9361 nnns volume:36 pages:241-255 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2004 GBV_ILN_2014 GBV_ILN_2068 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 36 241-255 |
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10.1016/j.cja.2022.08.014 doi (DE-627)ELV008998914 (ELSEVIER)S1000-9361(22)00184-4 DE-627 ger DE-627 rda eng 380 DE-600 6,25 ssgn ASIEN DE-1a fid LI, Peiran verfasserin aut Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft WEN, Xin verfasserin aut LIU, Haiying verfasserin aut LU, Yuping verfasserin aut Enthalten in Chinese journal of aeronautics Amsterdam [u.a.] : Elsevier, 2002 36, Seite 241-255 Online-Ressource (DE-627)534059384 (DE-600)2365081-3 (DE-576)267763506 1000-9361 nnns volume:36 pages:241-255 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2004 GBV_ILN_2014 GBV_ILN_2068 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 36 241-255 |
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LI, Peiran |
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LI, Peiran ddc 380 ssgn 6,25 fid ASIEN misc Attitude control misc Cooperative communication misc Discrete time control systems misc Multi agent systems misc Spacecraft Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference |
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380 DE-600 6,25 ssgn ASIEN DE-1a fid Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference Attitude control Cooperative communication Discrete time control systems Multi agent systems Spacecraft |
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event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference |
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Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference |
| abstract |
This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. |
| abstractGer |
This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. |
| abstract_unstemmed |
This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. |
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|
| score |
7.399952 |