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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 PublicationIEEE Transactions on Neural Networks and Learning Systems
ISSN2162-237X
Volume31Issue: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.

KeywordAttitude Control Bilevel Structure Deep Neural Network (Dnn) Six-degree-of-freedom (6-dof) Hypersonic Vehicle (Hv) Trajectory Planning
DOI10.1109/TNNLS.2019.2955400
URLView the original
Indexed BySCIE
Language英語English
WOS Research AreaComputer Science ; Engineering
WOS SubjectComputer Science, Artificial Intelligence ; Computer Science, Hardware & Architecture ; Computer Science, Theory & Methods ; Engineering, Electrical & Electronic
WOS IDWOS:000587699700048
PublisherIEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC, 445 HOES LANE, PISCATAWAY, NJ 08855-4141
Scopus ID2-s2.0-85089138365
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Document TypeJournal article
CollectionFaculty of Science and Technology
Corresponding AuthorChai, Runqi
Affiliation1.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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