Optimal satellite attitude control: A geometric approach

Nadjim Horri, Phil Palmer

Research output: Contribution to conferencePaper

12 Citations (Scopus)

Abstract

Optimal nonlinear control remains one of the most challenging subjects in control theory despite a long research history. In this paper, we present a geometric optimal control approach, which circumvents the tedious task of numerically solving online the Hamilton Jacobi Bellman (HJB) partial differential equation, which represents the dynamic programming formulation of the nonlinear global optimal control problem. Our approach makes implementation of nonlinear optimal attitude control practically feasible with low computational demand onboard a satellite. Optimal stabilizing state feedbacks are obtained from the construction of a Control Lyapunov function. Based on a phase space analysis, two natural dual optimal control objectives are considered to illustrate the application of this approach to satellite attitude control: Minimizing the norm of the control torque subject to a constraint on the convergence rate of a Lyapunov function, then maximizing the convergence rate of a Lyapunov function subject to a constraint on the control torque. Both approaches provide ease of implementation and achieve robust optimal trade-offs between attitude control rapidity and torque expenditure, without computational issues.
Original languageEnglish
DOIs
Publication statusPublished - 2009
Event2009 IEEE Aerospace Conference - Montana, Big Sky, United States
Duration: 7 Mar 200914 Mar 2009
http://ieeexplore.ieee.org/document/4839540/

Conference

Conference2009 IEEE Aerospace Conference
CountryUnited States
CityBig Sky
Period7/03/0914/03/09
Internet address

Fingerprint

Attitude control
Satellites
Lyapunov functions
Torque control
State feedback
Control theory
Dynamic programming
Partial differential equations
Torque
History

Keywords

  • Satellites
  • Optimal control
  • Lyapunov method
  • Torque control
  • Convergence
  • Control theory
  • History
  • Jacobian matrices
  • Partial differential equations
  • Dynamic programming

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Horri, N., & Palmer, P. (2009). Optimal satellite attitude control: A geometric approach. Paper presented at 2009 IEEE Aerospace Conference, Big Sky, United States. https://doi.org/10.1109/AERO.2009.4839540

Optimal satellite attitude control: A geometric approach. / Horri, Nadjim; Palmer, Phil .

2009. Paper presented at 2009 IEEE Aerospace Conference, Big Sky, United States.

Research output: Contribution to conferencePaper

Horri, N & Palmer, P 2009, 'Optimal satellite attitude control: A geometric approach' Paper presented at 2009 IEEE Aerospace Conference, Big Sky, United States, 7/03/09 - 14/03/09, . https://doi.org/10.1109/AERO.2009.4839540
Horri N, Palmer P. Optimal satellite attitude control: A geometric approach. 2009. Paper presented at 2009 IEEE Aerospace Conference, Big Sky, United States. https://doi.org/10.1109/AERO.2009.4839540
Horri, Nadjim ; Palmer, Phil . / Optimal satellite attitude control: A geometric approach. Paper presented at 2009 IEEE Aerospace Conference, Big Sky, United States.
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