Skip to main content
Top

2016 | OriginalPaper | Chapter

28. Attitude Control for Rigid Satellite Under Actuator Constraint

Authors : Aihua Zhang, Haitao Meng, Zhiqiang Zhang

Published in: Proceedings of the 2015 Chinese Intelligent Systems Conference

Publisher: Springer Berlin Heidelberg

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

An attitude controller is proposed via employing backstepping control technique, and being represented by modified Rodriguez parameters. A general dynamic attitude model of satellites is deduced, along with a general model of actuator dynamics which can describe presumably all actuators for space application. External disturbances and actuator constraints are explicitly addressed. The control performance is proved in the numerical simulation experiences at last.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Springer Professional "Wirtschaft"

Online-Abonnement

Mit Springer Professional "Wirtschaft" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 340 Zeitschriften

aus folgenden Fachgebieten:

  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Versicherung + Risiko




Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Yoon H, Agrawal BN (2009) Adaptive control of uncertain Hamiltonian multi-input multi-output systems: with application to spacecraft control. IEEE Trans Control Syst Technol 17:900–906 Yoon H, Agrawal BN (2009) Adaptive control of uncertain Hamiltonian multi-input multi-output systems: with application to spacecraft control. IEEE Trans Control Syst Technol 17:900–906
2.
go back to reference Seo D, Akella MR (2007) Separation property for the rigid body attitude tracking control problem. J Guidance Control Dyn 30:1569–1576 Seo D, Akella MR (2007) Separation property for the rigid body attitude tracking control problem. J Guidance Control Dyn 30:1569–1576
3.
go back to reference Seo D, Akella MR (2008) High-performance spacecraft adaptive attitude-tracking control through attracting-manifold design. J Guidance Control Dyn 31:884–891 Seo D, Akella MR (2008) High-performance spacecraft adaptive attitude-tracking control through attracting-manifold design. J Guidance Control Dyn 31:884–891
4.
go back to reference Plestan F, Bregeault V, Glumineau A, Shtessel Y, Moulay E (2012) Advances in high order and adaptive sliding mode control–theory and applications. In: Sliding modes after the first decade of the 21st century. Springer, 2012, pp 465–492 Plestan F, Bregeault V, Glumineau A, Shtessel Y, Moulay E (2012) Advances in high order and adaptive sliding mode control–theory and applications. In: Sliding modes after the first decade of the 21st century. Springer, 2012, pp 465–492
5.
go back to reference Sidi MJ (1997) Spacecraft dynamics and control: a practical engineering approach, vol 7. Cambridge University Press, Cambridge Sidi MJ (1997) Spacecraft dynamics and control: a practical engineering approach, vol 7. Cambridge University Press, Cambridge
6.
go back to reference Sekara TB, Matausek MR (2009) Optimization of PID controller based on maximization of the proportional gain under constraints on robustness and sensitivity to measurement noise. IEEE Trans Autom Control 54:184–189MathSciNetCrossRef Sekara TB, Matausek MR (2009) Optimization of PID controller based on maximization of the proportional gain under constraints on robustness and sensitivity to measurement noise. IEEE Trans Autom Control 54:184–189MathSciNetCrossRef
7.
go back to reference Zou A-M, Kumar KD, Hou Z-G (2010) Quaternion-based adaptive output feedback attitude control of spacecraft using Chebyshev neural networks. IEEE Trans Neural Netw 21:1457–1471CrossRef Zou A-M, Kumar KD, Hou Z-G (2010) Quaternion-based adaptive output feedback attitude control of spacecraft using Chebyshev neural networks. IEEE Trans Neural Netw 21:1457–1471CrossRef
8.
go back to reference Yin S, Ding S, Xie X, Luo H (2014) A review on basic data-driven approaches for industrial process monitoring. IEEE Trans Industr Electron 61:6418–6428CrossRef Yin S, Ding S, Xie X, Luo H (2014) A review on basic data-driven approaches for industrial process monitoring. IEEE Trans Industr Electron 61:6418–6428CrossRef
9.
go back to reference Crassidis JL, Markley FL (1996) Sliding mode control using modified Rodrigues parameters. J Guidance Control Dyn 19:1381–1383 Crassidis JL, Markley FL (1996) Sliding mode control using modified Rodrigues parameters. J Guidance Control Dyn 19:1381–1383
10.
go back to reference Sidi MJ (1997) Spacecraft dynamics and control. Cambridge University Press, CambridgeCrossRef Sidi MJ (1997) Spacecraft dynamics and control. Cambridge University Press, CambridgeCrossRef
11.
go back to reference Schaub H, Akella MR, Junkins JL (2001) Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics. J Guidance Control Dyn 24:95–100 Schaub H, Akella MR, Junkins JL (2001) Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics. J Guidance Control Dyn 24:95–100
Metadata
Title
Attitude Control for Rigid Satellite Under Actuator Constraint
Authors
Aihua Zhang
Haitao Meng
Zhiqiang Zhang
Copyright Year
2016
Publisher
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-662-48365-7_28

Premium Partner