Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation
As the number of satellites in orbit increases, the issue of flight safety in spacecraft formation orbit control has become increasingly prominent. With this in mind, this paper designs a second-order terminal sliding mode controller for spacecraft formation obstacle avoidance based on an artificial...
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MDPI AG
2023-07-01
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Series: | Electronics |
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Online Access: | https://www.mdpi.com/2079-9292/12/14/3179 |
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author | Ji Zhang Yili Wang Jun Jia Chuanguo Chi Huayi Li |
author_facet | Ji Zhang Yili Wang Jun Jia Chuanguo Chi Huayi Li |
author_sort | Ji Zhang |
collection | DOAJ |
description | As the number of satellites in orbit increases, the issue of flight safety in spacecraft formation orbit control has become increasingly prominent. With this in mind, this paper designs a second-order terminal sliding mode controller for spacecraft formation obstacle avoidance based on an artificial potential function (APF). To demonstrate the effectiveness of the controller, this paper first constructs a Lyapunov function to prove its stability and then verifies its theoretical validity through numerical simulation. Finally, a satellite simulator is used for semi-physical simulation to verify the practical effectiveness of the controller proposed in this paper. |
first_indexed | 2024-03-11T01:07:30Z |
format | Article |
id | doaj.art-32a252fd66904e3ba9377b52a2656d2d |
institution | Directory Open Access Journal |
issn | 2079-9292 |
language | English |
last_indexed | 2024-03-11T01:07:30Z |
publishDate | 2023-07-01 |
publisher | MDPI AG |
record_format | Article |
series | Electronics |
spelling | doaj.art-32a252fd66904e3ba9377b52a2656d2d2023-11-18T19:07:01ZengMDPI AGElectronics2079-92922023-07-011214317910.3390/electronics12143179Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical SimulationJi Zhang0Yili Wang1Jun Jia2Chuanguo Chi3Huayi Li4Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaShanghai Electro-Mechanical Engineering Institute, Shanghai 201109, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaAs the number of satellites in orbit increases, the issue of flight safety in spacecraft formation orbit control has become increasingly prominent. With this in mind, this paper designs a second-order terminal sliding mode controller for spacecraft formation obstacle avoidance based on an artificial potential function (APF). To demonstrate the effectiveness of the controller, this paper first constructs a Lyapunov function to prove its stability and then verifies its theoretical validity through numerical simulation. Finally, a satellite simulator is used for semi-physical simulation to verify the practical effectiveness of the controller proposed in this paper.https://www.mdpi.com/2079-9292/12/14/3179spacecraft formationsecond-order terminal sliding mode controllerobstacle avoidanceartificial potential functionsatellite simulator |
spellingShingle | Ji Zhang Yili Wang Jun Jia Chuanguo Chi Huayi Li Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation Electronics spacecraft formation second-order terminal sliding mode controller obstacle avoidance artificial potential function satellite simulator |
title | Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation |
title_full | Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation |
title_fullStr | Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation |
title_full_unstemmed | Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation |
title_short | Collision Avoidance Second Order Sliding Mode Control of Satellite Formation with Air-Floated Platform Semi-Physical Simulation |
title_sort | collision avoidance second order sliding mode control of satellite formation with air floated platform semi physical simulation |
topic | spacecraft formation second-order terminal sliding mode controller obstacle avoidance artificial potential function satellite simulator |
url | https://www.mdpi.com/2079-9292/12/14/3179 |
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