A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback

Amit Ailon; Reuven Segev; Shai Arogeti

doi:10.1109/TAC.2003.821406

A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback

Amit Ailon, Reuven Segev, Shai Arogeti

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

52 Scopus citations

Abstract

In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.

Original language	English
Pages (from-to)	125-130
Number of pages	6
Journal	IEEE Transactions on Automatic Control
Volume	49
Issue number	1
DOIs	https://doi.org/10.1109/TAC.2003.821406
State	Published - 1 Jan 2004

Keywords

Attitude regulation
Exponential stability
Region of attraction
Spacecraft
Time-delay
Velocity-free controller

ASJC Scopus subject areas

Control and Systems Engineering
Computer Science Applications
Electrical and Electronic Engineering

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10.1109/TAC.2003.821406

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abstract = "In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.",

keywords = "Attitude regulation, Exponential stability, Region of attraction, Spacecraft, Time-delay, Velocity-free controller",

author = "Amit Ailon and Reuven Segev and Shai Arogeti",

note = "Funding Information: Manuscript received July 17, 2001; revised April 29, 2002 and October 14, 2002. Recommended by Associate Editor K. M. Grigoriadis. This work was supported in part by the Israeli Ministry of Science under Grant 85962201 within the framework of the Israeli–Korean agreement on scientific cooperation in aerospace technology.",

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N2 - In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.

AB - In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.

KW - Attitude regulation

KW - Exponential stability

KW - Region of attraction

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KW - Time-delay

KW - Velocity-free controller

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A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback

Abstract

Keywords

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