Altitude control of a satellite using a feedback linearization

M. Benenia; H. Batatia; F. Mora Camino; M. Benslama

doi:10.1049/cp.2013.0018

Altitude control of a satellite using a feedback linearization

M. Benenia
, H. Batatia
, F. Mora Camino
, M. Benslama

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

2 Citations (Scopus)

Abstract

This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.

Original language	English
Title of host publication	IET Conference on Control and Automation 2013
Subtitle of host publication	Uniting Problems and Solutions
Publisher	Institution of Engineering and Technology
ISBN (Electronic)	9781849197106
DOIs	https://doi.org/10.1049/cp.2013.0018
Publication status	Published - 2013
Event	2013 IET Conference on Control and Automation: Uniting Problems and Solutions - Birmingham, United Kingdom Duration: 4 Jun 2013 → 5 Jun 2013

Conference

Conference	2013 IET Conference on Control and Automation: Uniting Problems and Solutions
Country/Territory	United Kingdom
City	Birmingham
Period	4/06/13 → 5/06/13

Keywords

Feedback linearization
Quaternion
Sliding mode control
Spacecraft attitude control

ASJC Scopus subject areas

Control and Optimization
Modelling and Simulation

Access to Document

10.1049/cp.2013.0018

Cite this

@inproceedings{e55a39ce8cd44f94a8a45e6d25d94188,

title = "Altitude control of a satellite using a feedback linearization",

abstract = "This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.",

keywords = "Feedback linearization, Quaternion, Sliding mode control, Spacecraft attitude control",

author = "M. Benenia and H. Batatia and Camino, \{F. Mora\} and M. Benslama",

year = "2013",

doi = "10.1049/cp.2013.0018",

language = "English",

booktitle = "IET Conference on Control and Automation 2013",

publisher = "Institution of Engineering and Technology",

address = "United Kingdom",

note = "2013 IET Conference on Control and Automation: Uniting Problems and Solutions ; Conference date: 04-06-2013 Through 05-06-2013",

}

Benenia, M, Batatia, H, Camino, FM & Benslama, M 2013, Altitude control of a satellite using a feedback linearization. in IET Conference on Control and Automation 2013: Uniting Problems and Solutions., 18, Institution of Engineering and Technology, 2013 IET Conference on Control and Automation: Uniting Problems and Solutions, Birmingham, United Kingdom, 4/06/13. https://doi.org/10.1049/cp.2013.0018

TY - GEN

T1 - Altitude control of a satellite using a feedback linearization

AU - Benenia, M.

AU - Batatia, H.

AU - Camino, F. Mora

AU - Benslama, M.

PY - 2013

Y1 - 2013

N2 - This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.

AB - This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.

KW - Feedback linearization

KW - Quaternion

KW - Sliding mode control

KW - Spacecraft attitude control

UR - https://www.scopus.com/pages/publications/85085406050

U2 - 10.1049/cp.2013.0018

DO - 10.1049/cp.2013.0018

M3 - Conference contribution

AN - SCOPUS:85085406050

BT - IET Conference on Control and Automation 2013

PB - Institution of Engineering and Technology

T2 - 2013 IET Conference on Control and Automation: Uniting Problems and Solutions

Y2 - 4 June 2013 through 5 June 2013

ER -

Altitude control of a satellite using a feedback linearization

Abstract

Conference

Keywords

ASJC Scopus subject areas

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