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Model predictive control guidance for constrained mars pinpoint landing

Model predictive control guidance for constrained mars pinpoint landing
Model predictive control guidance for constrained mars pinpoint landing
In order to achieve pinpoint landing under various constraints during powered descent phase of landing on Mars, model predictive control (MPC) is employed in this paper by designing a novel performance index. Its main advantage is that it can ensure the pinpoint landing with online calculation and handle constraints as well, both of which are important in practical engineering missions. Detailed derivational process is given. Simulation results show the effectiveness of the proposed guidance.
Geometrical constraints, Model predictive control, Pinpoint landing, Powered descent phase
201-206
IEEE
Wang, Ting
14031e6d-9db2-4ac9-94ea-e7f80c24452d
Guo, Yanning
8c00e47f-af8f-4897-97ea-06160d66a914
Zhang, Yao
a4f30318-ab42-4b38-a60d-f7199ff3a02a
Ma, Guangfu
c6a689cd-bd7e-4b86-b297-6d6bbf2a9343
Liang, Zimu
634e5883-8ae8-4cc6-92a5-f4240f171bd8
Wang, Ting
14031e6d-9db2-4ac9-94ea-e7f80c24452d
Guo, Yanning
8c00e47f-af8f-4897-97ea-06160d66a914
Zhang, Yao
a4f30318-ab42-4b38-a60d-f7199ff3a02a
Ma, Guangfu
c6a689cd-bd7e-4b86-b297-6d6bbf2a9343
Liang, Zimu
634e5883-8ae8-4cc6-92a5-f4240f171bd8

Wang, Ting, Guo, Yanning, Zhang, Yao, Ma, Guangfu and Liang, Zimu (2016) Model predictive control guidance for constrained mars pinpoint landing. In Proceedings of 2016 2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016. IEEE. pp. 201-206 . (doi:10.1109/CCSSE.2016.7784382).

Record type: Conference or Workshop Item (Paper)

Abstract

In order to achieve pinpoint landing under various constraints during powered descent phase of landing on Mars, model predictive control (MPC) is employed in this paper by designing a novel performance index. Its main advantage is that it can ensure the pinpoint landing with online calculation and handle constraints as well, both of which are important in practical engineering missions. Detailed derivational process is given. Simulation results show the effectiveness of the proposed guidance.

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More information

Published date: 14 December 2016
Additional Information: Funding Information: This work is supported partially by National Basic Research Program of China (Grant No.2012CB720000), the National Natural Science Foundation of China (Grant No.,61304005,61403103), China Postdoctoral Science Foundation(Grant No. 2014M550195), and Fundamental Research Funds for the Central Universities (Grant No.HIT.NSRIF.2014035,2014139). Publisher Copyright:© 2016 IEEE.
Venue - Dates: 2nd International Conference on Control Science and Systems Engineering, ICCSSE 2016, , Singapore, Singapore, 2016-07-27 - 2016-07-29
Keywords: Geometrical constraints, Model predictive control, Pinpoint landing, Powered descent phase

Identifiers

Local EPrints ID: 472382
URI: http://eprints.soton.ac.uk/id/eprint/472382
PURE UUID: 56722365-6843-4033-aee1-abbeb9c89438
ORCID for Yao Zhang: ORCID iD orcid.org/0000-0002-3821-371X

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Date deposited: 02 Dec 2022 17:47
Last modified: 18 Mar 2024 04:07

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Contributors

Author: Ting Wang
Author: Yanning Guo
Author: Yao Zhang ORCID iD
Author: Guangfu Ma
Author: Zimu Liang

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