Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach
Joint Authors
Chen, Kang
Fu, Bin
Ding, Yuening
Yan, Jie
Source
Mathematical Problems in Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-19, 19 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-08-27
Country of Publication
Egypt
No. of Pages
19
Main Subjects
Abstract EN
This paper focuses on the integrated guidance and control (IGC) method applied in the interception of maneuvering near space hypersonic vehicles using the homogeneous high order sliding mode (HOSM) approach.
The IGC model is derived by combining the target-missile relative motion and dynamic equations.
Then, a fourth-order sliding mode controller is implemented in the augmented IGC model.
To estimate the high order derivatives of the sliding manifold which is required in the HOSM method, an Arbitrary Order Robust Exact Differentiator is presented.
At last, the idea of virtual control is introduced to alleviate the chattering of the control input without using any saturation functions which may lead to a loss of the robustness.
And the stability of the closed-loop system with presented fourth-order homogeneous HOSM controller is also proved theoretically.
Finally, simulation results are provided and analyzed to demonstrate the effectiveness of the proposed method in three typical engagement scenarios.
American Psychological Association (APA)
Chen, Kang& Fu, Bin& Ding, Yuening& Yan, Jie. 2015. Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach. Mathematical Problems in Engineering،Vol. 2015, no. 2015, pp.1-19.
https://search.emarefa.net/detail/BIM-1074388
Modern Language Association (MLA)
Chen, Kang…[et al.]. Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach. Mathematical Problems in Engineering No. 2015 (2015), pp.1-19.
https://search.emarefa.net/detail/BIM-1074388
American Medical Association (AMA)
Chen, Kang& Fu, Bin& Ding, Yuening& Yan, Jie. Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach. Mathematical Problems in Engineering. 2015. Vol. 2015, no. 2015, pp.1-19.
https://search.emarefa.net/detail/BIM-1074388
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1074388