Adaptive Prescribed-time Control for Coupled 6-DOF Spacecraft Formation Flying
This paper studies the prescribed-time spacecraft formation flying problem under known and unknown external disturbance. The coupled 6-degrees-of-freedom relative kinematics and dynamics for spacecraft are modeled by using exponential coordinates of SE(3). With the help of the linear time-varying Ly...
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| Veröffentlicht in: | International journal of control, automation, and systems automation, and systems, 2023-02, Vol.21 (2), p.350-358 |
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| container_title | International journal of control, automation, and systems |
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| creator | Chen, Li Sun, Yongyan Shao, Xiaowei Chen, Junli Zhang, Dexin |
| description | This paper studies the prescribed-time spacecraft formation flying problem under known and unknown external disturbance. The coupled 6-degrees-of-freedom relative kinematics and dynamics for spacecraft are modeled by using exponential coordinates of SE(3). With the help of the linear time-varying Lyapunov inequality based prescribed-time stability theorem, a novel global adaptive prescribed-time time-varying high-gain control law is designed by backstepping. It is shown that the designed controller is bounded. Numerical simulations verify the effectiveness of the proposed control method. |
| doi_str_mv | 10.1007/s12555-021-0671-2 |
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The coupled 6-degrees-of-freedom relative kinematics and dynamics for spacecraft are modeled by using exponential coordinates of SE(3). With the help of the linear time-varying Lyapunov inequality based prescribed-time stability theorem, a novel global adaptive prescribed-time time-varying high-gain control law is designed by backstepping. It is shown that the designed controller is bounded. 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Numerical simulations verify the effectiveness of the proposed control method.</description><subject>Adaptive control</subject><subject>Control</subject><subject>Control methods</subject><subject>Control systems design</subject><subject>Control theory</subject><subject>Degrees of freedom</subject><subject>Engineering</subject><subject>Formation flying</subject><subject>High gain</subject><subject>Kinematics</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Mechatronics</subject><subject>Regular Papers</subject><subject>Robotics</subject><subject>Spacecraft</subject><issn>1598-6446</issn><issn>2005-4092</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNp1kE1LwzAYx4MoOKcfwFvBc_RJ0qTLcUyrwnCCeg556-jompp0gt_ejAqePD3_w__l4YfQNYFbAlDdJUI55xgowSAqgukJmlEAjkuQ9BTNCJcLLMpSnKOLlHYAQlBZzdDL0ulhbL988Rp9srE13uGx3ftiFfoxhq5oQsz6MHTeFQLfb-ribdDW26ibsahD3OuxDX1Rd99tv71EZ43ukr_6vXP0UT-8r57wevP4vFqusWVEjNhbrj1wIs2xiVFjKBN5mTDZcJofaxpmpJcWjBBAqXMVWMuYNs4ZcILN0c3UO8TwefBpVLtwiH2eVLSqCAi5KHl2kcllY0gp-kYNsd3r-K0IqCM2NWFTGZs6YlM0Z-iUSdnbb338a_4_9AOxBW_Z</recordid><startdate>20230201</startdate><enddate>20230201</enddate><creator>Chen, Li</creator><creator>Sun, Yongyan</creator><creator>Shao, Xiaowei</creator><creator>Chen, Junli</creator><creator>Zhang, Dexin</creator><general>Institute of Control, Robotics and Systems and The Korean Institute of Electrical Engineers</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0002-2603-057X</orcidid></search><sort><creationdate>20230201</creationdate><title>Adaptive Prescribed-time Control for Coupled 6-DOF Spacecraft Formation Flying</title><author>Chen, Li ; Sun, Yongyan ; Shao, Xiaowei ; Chen, Junli ; Zhang, Dexin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c316t-ec5ae0519bacec32bb236bed139f52297ff3b9e9c0b66022dd70cc33abddb0d63</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Adaptive control</topic><topic>Control</topic><topic>Control methods</topic><topic>Control systems design</topic><topic>Control theory</topic><topic>Degrees of freedom</topic><topic>Engineering</topic><topic>Formation flying</topic><topic>High gain</topic><topic>Kinematics</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Mechatronics</topic><topic>Regular Papers</topic><topic>Robotics</topic><topic>Spacecraft</topic><toplevel>online_resources</toplevel><creatorcontrib>Chen, Li</creatorcontrib><creatorcontrib>Sun, Yongyan</creatorcontrib><creatorcontrib>Shao, Xiaowei</creatorcontrib><creatorcontrib>Chen, Junli</creatorcontrib><creatorcontrib>Zhang, Dexin</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>International journal of control, automation, and systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chen, Li</au><au>Sun, Yongyan</au><au>Shao, Xiaowei</au><au>Chen, Junli</au><au>Zhang, Dexin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Adaptive Prescribed-time Control for Coupled 6-DOF Spacecraft Formation Flying</atitle><jtitle>International journal of control, automation, and systems</jtitle><stitle>Int. J. Control Autom. Syst</stitle><date>2023-02-01</date><risdate>2023</risdate><volume>21</volume><issue>2</issue><spage>350</spage><epage>358</epage><pages>350-358</pages><issn>1598-6446</issn><eissn>2005-4092</eissn><abstract>This paper studies the prescribed-time spacecraft formation flying problem under known and unknown external disturbance. The coupled 6-degrees-of-freedom relative kinematics and dynamics for spacecraft are modeled by using exponential coordinates of SE(3). With the help of the linear time-varying Lyapunov inequality based prescribed-time stability theorem, a novel global adaptive prescribed-time time-varying high-gain control law is designed by backstepping. It is shown that the designed controller is bounded. 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| ispartof | International journal of control, automation, and systems, 2023-02, Vol.21 (2), p.350-358 |
| issn | 1598-6446 2005-4092 |
| language | eng |
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| source | SpringerNature Journals |
| subjects | Adaptive control Control Control methods Control systems design Control theory Degrees of freedom Engineering Formation flying High gain Kinematics Mathematical analysis Mathematical models Mechatronics Regular Papers Robotics Spacecraft |
| title | Adaptive Prescribed-time Control for Coupled 6-DOF Spacecraft Formation Flying |
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