Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations

Ming Zeng; Yunling Li; Hao An; Changhong Wang

doi:10.1109/CoDIT.2018.8394821

Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations

Ming Zeng
, Yunling Li
, Hao An
, Changhong Wang^*

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In this paper, a prescribed performance control (PPC) is proposed for hypersonic flight vehicles (HFVs) in the presence of uncertainties and input saturations. A simplified error transformation is implemented to relax the constraints on the tracking performance, including overshoot, convergence rate and steady-state error. The stabilization of the transformed system is sufficient to achieve the prescribed performance. Based on the transformed error, a novel auxiliary system combined with the adaptive control is constructed to analyze and then compensate for the effect of input saturations. Simulation is provided to verify the effectiveness of the proposed scheme.

Original language	English
Title of host publication	2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	641-646
Number of pages	6
ISBN (Electronic)	9781538650653
DOIs	https://doi.org/10.1109/CoDIT.2018.8394821
State	Published - 22 Jun 2018
Event	5th International Conference on Control, Decision and Information Technologies, CoDIT 2018 - Thessaloniki, Greece Duration: 10 Apr 2018 → 13 Apr 2018

Publication series

Name	2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018

Conference

Conference	5th International Conference on Control, Decision and Information Technologies, CoDIT 2018
Country/Territory	Greece
City	Thessaloniki
Period	10/04/18 → 13/04/18

Access to Document

10.1109/CoDIT.2018.8394821

Cite this

Zeng, M., Li, Y., An, H., & Wang, C. (2018). Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations. In 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018 (pp. 641-646). (2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CoDIT.2018.8394821

Zeng, Ming ; Li, Yunling ; An, Hao et al. / Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations. 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018. Institute of Electrical and Electronics Engineers Inc., 2018. pp. 641-646 (2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018).

@inproceedings{41e347c9869942328e318ba844ef4e0e,

title = "Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations",

abstract = "In this paper, a prescribed performance control (PPC) is proposed for hypersonic flight vehicles (HFVs) in the presence of uncertainties and input saturations. A simplified error transformation is implemented to relax the constraints on the tracking performance, including overshoot, convergence rate and steady-state error. The stabilization of the transformed system is sufficient to achieve the prescribed performance. Based on the transformed error, a novel auxiliary system combined with the adaptive control is constructed to analyze and then compensate for the effect of input saturations. Simulation is provided to verify the effectiveness of the proposed scheme.",

author = "Ming Zeng and Yunling Li and Hao An and Changhong Wang",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018 ; Conference date: 10-04-2018 Through 13-04-2018",

year = "2018",

month = jun,

day = "22",

doi = "10.1109/CoDIT.2018.8394821",

language = "英语",

series = "2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018",

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pages = "641--646",

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address = "美国",

}

Zeng, M, Li, Y, An, H & Wang, C 2018, Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations. in 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018. 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018, Institute of Electrical and Electronics Engineers Inc., pp. 641-646, 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018, Thessaloniki, Greece, 10/04/18. https://doi.org/10.1109/CoDIT.2018.8394821

Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations. / Zeng, Ming; Li, Yunling; An, Hao et al.
2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018. Institute of Electrical and Electronics Engineers Inc., 2018. p. 641-646 (2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - An, Hao

AU - Wang, Changhong

PY - 2018/6/22

Y1 - 2018/6/22

N2 - In this paper, a prescribed performance control (PPC) is proposed for hypersonic flight vehicles (HFVs) in the presence of uncertainties and input saturations. A simplified error transformation is implemented to relax the constraints on the tracking performance, including overshoot, convergence rate and steady-state error. The stabilization of the transformed system is sufficient to achieve the prescribed performance. Based on the transformed error, a novel auxiliary system combined with the adaptive control is constructed to analyze and then compensate for the effect of input saturations. Simulation is provided to verify the effectiveness of the proposed scheme.

AB - In this paper, a prescribed performance control (PPC) is proposed for hypersonic flight vehicles (HFVs) in the presence of uncertainties and input saturations. A simplified error transformation is implemented to relax the constraints on the tracking performance, including overshoot, convergence rate and steady-state error. The stabilization of the transformed system is sufficient to achieve the prescribed performance. Based on the transformed error, a novel auxiliary system combined with the adaptive control is constructed to analyze and then compensate for the effect of input saturations. Simulation is provided to verify the effectiveness of the proposed scheme.

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BT - 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018

PB - Institute of Electrical and Electronics Engineers Inc.

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ER -

Zeng M, Li Y, An H , Wang C. Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations. In 2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018. Institute of Electrical and Electronics Engineers Inc. 2018. p. 641-646. (2018 5th International Conference on Control, Decision and Information Technologies, CoDIT 2018). doi: 10.1109/CoDIT.2018.8394821

Performance-Guaranteed Robust Control of Hypersonic Flight Vehicles subject to Input Saturations

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