Fixed-Time Planetary Landing Guidance With Unknown Disturbance and Thruster Constraint
This article proposes a planetary autonomous soft pinpoint adaptive fixed-time feedback landing guidance scheme based on the sliding mode control that is subject to thruster magnitude constraint, unknown control acceleration deviation, and disturbance without a priori knowledge. More specifically, a...
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| Published in | IEEE transactions on aerospace and electronic systems Vol. 59; no. 1; pp. 483 - 496 |
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| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
| Published |
New York
IEEE
01.02.2023
The Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0018-9251 1557-9603 |
| DOI | 10.1109/TAES.2022.3183961 |
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| Abstract | This article proposes a planetary autonomous soft pinpoint adaptive fixed-time feedback landing guidance scheme based on the sliding mode control that is subject to thruster magnitude constraint, unknown control acceleration deviation, and disturbance without a priori knowledge. More specifically, a sliding surface is designed, and its gain is adjusted by the system state, increasing the convergence rate. Then, the adaptive law is proposed to compensate for the thruster magnitude constraint, unknown control acceleration deviation, and disturbance without a priori knowledge. On these bases, a thruster-magnitude-constrained feedback landing guidance is developed to ensure the fixed-time stability of the vehicle even in the presence of unknown control acceleration deviation and disturbance without priori knowledge. Furthermore, numerical simulations are performed to verify the feasibility and effectiveness of the proposed algorithms. Moreover, its near-fuel-optimal performance is illustrated by comparing it with offline fuel-optimal guidance. |
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| AbstractList | This article proposes a planetary autonomous soft pinpoint adaptive fixed-time feedback landing guidance scheme based on the sliding mode control that is subject to thruster magnitude constraint, unknown control acceleration deviation, and disturbance without a priori knowledge. More specifically, a sliding surface is designed, and its gain is adjusted by the system state, increasing the convergence rate. Then, the adaptive law is proposed to compensate for the thruster magnitude constraint, unknown control acceleration deviation, and disturbance without a priori knowledge. On these bases, a thruster-magnitude-constrained feedback landing guidance is developed to ensure the fixed-time stability of the vehicle even in the presence of unknown control acceleration deviation and disturbance without priori knowledge. Furthermore, numerical simulations are performed to verify the feasibility and effectiveness of the proposed algorithms. Moreover, its near-fuel-optimal performance is illustrated by comparing it with offline fuel-optimal guidance. |
| Author | Guo, Yanning Ma, Guangfu Li, Dongyu Gong, Youmin Guo, Minwen |
| Author_xml | – sequence: 1 givenname: Youmin orcidid: 0000-0002-1865-5414 surname: Gong fullname: Gong, Youmin email: hitgym@163.com organization: Department of Control Science and Engineering, Harbin Institute of Technology, Harbin, China – sequence: 2 givenname: Yanning orcidid: 0000-0001-6150-3646 surname: Guo fullname: Guo, Yanning email: guoyn@hit.edu.cn organization: Department of Control Science and Engineering, Harbin Institute of Technology, Harbin, China – sequence: 3 givenname: Dongyu orcidid: 0000-0001-8338-0536 surname: Li fullname: Li, Dongyu email: dongyulevyli@gmail.com organization: School of Cyber Science and Technology, Beihang University, Beijing, China – sequence: 4 givenname: Guangfu orcidid: 0000-0002-4654-9045 surname: Ma fullname: Ma, Guangfu email: magf@hit.edu.cn organization: Department of Control Science and Engineering, Harbin Institute of Technology, Harbin, China – sequence: 5 givenname: Minwen orcidid: 0000-0003-2147-1832 surname: Guo fullname: Guo, Minwen email: mwguo8500@163.com organization: Beijing Institute of Control Engineering, Beijing, China |
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| Snippet | This article proposes a planetary autonomous soft pinpoint adaptive fixed-time feedback landing guidance scheme based on the sliding mode control that is... |
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| SubjectTerms | Adaptive control Adaptive systems Algorithms Attitude control Constraints Convergence Deviation Feedback Fixed-time stable Fuels Mars Navigation Planetary landing planetary landing guidance Robustness Sliding mode control thruster magnitude constraint unknown control deviation unknown disturbance |
| Title | Fixed-Time Planetary Landing Guidance With Unknown Disturbance and Thruster Constraint |
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