Residential College | false |
Status | 已發表Published |
Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach | |
Chai, Runqi1; Tsourdos, Antonios1; Savvaris, Al1; Chai, Senchun2; Xia, Yuanqing2; Chen, C. L.Philip3,4,5 | |
2020-11-01 | |
Source Publication | IEEE Transactions on Neural Networks and Learning Systems |
ISSN | 2162-237X |
Volume | 31Issue:11Pages:5005-5013 |
Abstract | This brief presents an integrated trajectory planning and attitude control framework for six-degree-of-freedom (6-DOF) hypersonic vehicle (HV) reentry flight. The proposed framework utilizes a bilevel structure incorporating desensitized trajectory optimization and deep neural network (DNN)-based control. In the upper level, a trajectory data set containing optimal system control and state trajectories is generated, while in the lower level control system, DNNs are constructed and trained using the pregenerated trajectory ensemble in order to represent the functional relationship between the optimized system states and controls. These well-trained networks are then used to produce optimal feedback actions online. A detailed simulation analysis was performed to validate the real-time applicability and the optimality of the designed bilevel framework. Moreover, a comparative analysis was also carried out between the proposed DNN-driven controller and other optimization-based techniques existing in related works. Our results verify the reliability of using the proposed bilevel design for the control of HV reentry flight in real time. |
Keyword | Attitude Control Bilevel Structure Deep Neural Network (Dnn) Six-degree-of-freedom (6-dof) Hypersonic Vehicle (Hv) Trajectory Planning |
DOI | 10.1109/TNNLS.2019.2955400 |
URL | View the original |
Indexed By | SCIE |
Language | 英語English |
WOS Research Area | Computer Science ; Engineering |
WOS Subject | Computer Science, Artificial Intelligence ; Computer Science, Hardware & Architecture ; Computer Science, Theory & Methods ; Engineering, Electrical & Electronic |
WOS ID | WOS:000587699700048 |
Publisher | IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC, 445 HOES LANE, PISCATAWAY, NJ 08855-4141 |
Scopus ID | 2-s2.0-85089138365 |
Fulltext Access | |
Citation statistics | |
Document Type | Journal article |
Collection | Faculty of Science and Technology |
Corresponding Author | Chai, Runqi |
Affiliation | 1.School of Aerospace, Transport and Manufacturing, Cranfield University, Bedford, MK43 0AL, United Kingdom 2.School of Automation, Beijing Institute of Technology, Beijing, 100811, China 3.Faculty of Science and Technology, University of Macau, 999078, Macao 4.Department of Navigation, Dalian Maritime University, Dalian, 116026, China 5.State Key Laboratory of Management and Control for Complex Systems, Institute of Automation, Chinese Academy of Sciences, Beijing, 100080, China |
Recommended Citation GB/T 7714 | Chai, Runqi,Tsourdos, Antonios,Savvaris, Al,et al. Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach[J]. IEEE Transactions on Neural Networks and Learning Systems, 2020, 31(11), 5005-5013. |
APA | Chai, Runqi., Tsourdos, Antonios., Savvaris, Al., Chai, Senchun., Xia, Yuanqing., & Chen, C. L.Philip (2020). Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach. IEEE Transactions on Neural Networks and Learning Systems, 31(11), 5005-5013. |
MLA | Chai, Runqi,et al."Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach".IEEE Transactions on Neural Networks and Learning Systems 31.11(2020):5005-5013. |
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