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Multi-power sliding mode guidance for Mars powered descent phase

Multi-power sliding mode guidance for Mars powered descent phase
Multi-power sliding mode guidance for Mars powered descent phase
To reach and keep tracking the desired Mars landing trajectory rapidly under various uncertainties and unexpected wind, a power reaching law based sliding mode tracking guidance algorithm is proposed in this paper. The proposed guidance law is composed of three exponential terms, its main improvement is that it can ensure that the lander track the reference trajectory in finite time without chattering. Theoretical proofs are presented to prove its existence, reachability and stabilization characteristics. Compared with existing exponential reaching law, single power reaching law and double power reaching law, simulation results show the effectiveness of the proposed guidance law with a typical Mars powered descent landing scenario
Guo, Yanning
8c00e47f-af8f-4897-97ea-06160d66a914
Zhang, Yao
a4f30318-ab42-4b38-a60d-f7199ff3a02a
Ma, Guangfu
dd3ce7d7-b1e5-445a-a6f2-5107024dd80f
Zeng, Tianyi
0c259925-4a87-4aaf-b373-215f65c56298
Guo, Yanning
8c00e47f-af8f-4897-97ea-06160d66a914
Zhang, Yao
a4f30318-ab42-4b38-a60d-f7199ff3a02a
Ma, Guangfu
dd3ce7d7-b1e5-445a-a6f2-5107024dd80f
Zeng, Tianyi
0c259925-4a87-4aaf-b373-215f65c56298

Guo, Yanning, Zhang, Yao, Ma, Guangfu and Zeng, Tianyi (2016) Multi-power sliding mode guidance for Mars powered descent phase. Control 2016 - 11th International Conference on Control, Queen's University, Belfast, United Kingdom. 31 Aug - 02 Sep 2016.

Record type: Conference or Workshop Item (Paper)

Abstract

To reach and keep tracking the desired Mars landing trajectory rapidly under various uncertainties and unexpected wind, a power reaching law based sliding mode tracking guidance algorithm is proposed in this paper. The proposed guidance law is composed of three exponential terms, its main improvement is that it can ensure that the lander track the reference trajectory in finite time without chattering. Theoretical proofs are presented to prove its existence, reachability and stabilization characteristics. Compared with existing exponential reaching law, single power reaching law and double power reaching law, simulation results show the effectiveness of the proposed guidance law with a typical Mars powered descent landing scenario

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More information

Published date: 2016
Venue - Dates: Control 2016 - 11th International Conference on Control, Queen's University, Belfast, United Kingdom, 2016-08-31 - 2016-09-02

Identifiers

Local EPrints ID: 477750
URI: http://eprints.soton.ac.uk/id/eprint/477750
PURE UUID: a9cde825-4238-4e24-86c5-d7922e47689c
ORCID for Yao Zhang: ORCID iD orcid.org/0000-0002-3821-371X

Catalogue record

Date deposited: 13 Jun 2023 17:33
Last modified: 14 Jun 2023 02:11

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Contributors

Author: Yanning Guo
Author: Yao Zhang ORCID iD
Author: Guangfu Ma
Author: Tianyi Zeng

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