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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Main Authors: Ji Zhang, Yili Wang, Jun Jia, Chuanguo Chi, Huayi Li
Format: Article
Language:English
Published: MDPI AG 2023-07-01
Series:Electronics
Subjects:
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.
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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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AT yiliwang collisionavoidancesecondorderslidingmodecontrolofsatelliteformationwithairfloatedplatformsemiphysicalsimulation
AT junjia collisionavoidancesecondorderslidingmodecontrolofsatelliteformationwithairfloatedplatformsemiphysicalsimulation
AT chuanguochi collisionavoidancesecondorderslidingmodecontrolofsatelliteformationwithairfloatedplatformsemiphysicalsimulation
AT huayili collisionavoidancesecondorderslidingmodecontrolofsatelliteformationwithairfloatedplatformsemiphysicalsimulation