Abstract
Because of particular dynamic characteristics, the traditional method for calculating weight matrices in LQR is not suitable for reentry vehicle profile-following. This paper designs parameter varying weight matrix. In this method, on the basis of vehicle entry flight characteristics, we design the functional relationship between weight matrix parameters and flight states. The simulations show that this method can improve the performance of reentry vehicle profile following obviously, and it is more robust to different disturbances.
Original language | English |
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Title of host publication | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
Editors | Shengyuan Xu, Qianchuan Zhao |
Publisher | IEEE Computer Society |
Pages | 1031-1034 |
Number of pages | 4 |
ISBN (Electronic) | 9789881563842 |
DOIs | |
Publication status | Published - 11 Sept 2014 |
Externally published | Yes |
Event | Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China Duration: 28 Jul 2014 → 30 Jul 2014 |
Publication series
Name | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
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ISSN (Print) | 1934-1768 |
ISSN (Electronic) | 2161-2927 |
Conference
Conference | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
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Country/Territory | China |
City | Nanjing |
Period | 28/07/14 → 30/07/14 |
Keywords
- LQR
- Reentry vehicle
- optimization
- profile following
- weight matrix
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Xiong, Z., Ren, Z., Liang, Z., & Bai, C. (2014). Optimization studies of weight matrix in LQR for reentry vehicle profile-following. In S. Xu, & Q. Zhao (Eds.), Proceedings of the 33rd Chinese Control Conference, CCC 2014 (pp. 1031-1034). Article 6896769 (Proceedings of the 33rd Chinese Control Conference, CCC 2014). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2014.6896769