Passivity-based attitude control with input quantization

Xiaoyu Lang; Christopher J. Damaren; Xibin Cao

doi:10.1177/0954410017754018

Passivity-based attitude control with input quantization

Xiaoyu Lang^*
, Christopher J. Damaren
, Xibin Cao

^*Corresponding author for this work

Harbin Institute of Technology
University of Toronto

Research output: Contribution to journal › Article › peer-review

9 Citations (Scopus)

Abstract

A passivity-based controller with quantization for spacecraft attitude control is developed. This passive control scheme includes two parts which are a proportional controller for quaternion feedback and a strictly positive real controller for the angular velocity. To alleviate the errors caused by quantization, a special modification for the nonlinear quantized input is employed in the strictly positive real controller. Asymptotic stability can be guaranteed with the presented controller structure. A guideline for the controller parameter selection is provided with sensitivity analysis for the control scheme. Numerical simulation results demonstrate the effectiveness of the proposed controller.

Original language	English
Pages (from-to)	1546-1551
Number of pages	6
Journal	Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Volume	233
Issue number	4
DOIs	https://doi.org/10.1177/0954410017754018
Publication status	Published - 1 Mar 2019
Externally published	Yes

Keywords

Passivity
attitude control
nonlinear modification
quantization
spacecraft

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10.1177/0954410017754018

Cite this

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keywords = "Passivity, attitude control, nonlinear modification, quantization, spacecraft",

author = "Xiaoyu Lang and Damaren, \{Christopher J.\} and Xibin Cao",

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AU - Damaren, Christopher J.

AU - Cao, Xibin

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PY - 2019/3/1

Y1 - 2019/3/1

N2 - A passivity-based controller with quantization for spacecraft attitude control is developed. This passive control scheme includes two parts which are a proportional controller for quaternion feedback and a strictly positive real controller for the angular velocity. To alleviate the errors caused by quantization, a special modification for the nonlinear quantized input is employed in the strictly positive real controller. Asymptotic stability can be guaranteed with the presented controller structure. A guideline for the controller parameter selection is provided with sensitivity analysis for the control scheme. Numerical simulation results demonstrate the effectiveness of the proposed controller.

AB - A passivity-based controller with quantization for spacecraft attitude control is developed. This passive control scheme includes two parts which are a proportional controller for quaternion feedback and a strictly positive real controller for the angular velocity. To alleviate the errors caused by quantization, a special modification for the nonlinear quantized input is employed in the strictly positive real controller. Asymptotic stability can be guaranteed with the presented controller structure. A guideline for the controller parameter selection is provided with sensitivity analysis for the control scheme. Numerical simulation results demonstrate the effectiveness of the proposed controller.

KW - Passivity

KW - attitude control

KW - nonlinear modification

KW - quantization

KW - spacecraft

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ER -

Passivity-based attitude control with input quantization

Abstract

Keywords

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