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Integrated guidance and control of elastic flight vehicle based on robust MPC

Shamaghdari, S ; Sharif University of Technology | 2015

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  1. Type of Document: Article
  2. DOI: 10.1002/rnc.3215
  3. Publisher: John Wiley and Sons Ltd , 2015
  4. Abstract:
  5. Integrated guidance and control of an elastic flight vehicle based on constrained robust model predictive control is proposed. The design is based on a partial state feedback control law that minimizes a cost function within the framework of linear matrix inequalities. It is shown that the solution of the defined optimization problem stabilizes the nonlinear plant. Nonlinear kinematics and dynamics are taken into account, and internal stability of the closed-loop nonlinear system is guaranteed. The performance and effectiveness of the proposed integrated guidance and control against non-maneuvering and weaving targets are evaluated using computer simulations
  6. Keywords:
  7. Elasticity, stability ; Integrated guidance and control ; Air navigation ; Amphibious vehicles ; Cost functions ; Feedback ; Feedback control ; Linear matrix inequalities ; Maneuverability ; Model predictive control ; Nonlinear systems ; Optimization ; Predictive control systems ; Robust control ; Robustness (control systems) ; State feedback ; System stability ; Vehicles ; Air vehicle ; Integrated guidance and controls ; Region of domination ; Robust model predictive control ; Aircraft control
  8. Source: International Journal of Robust and Nonlinear Control ; Volume 25, Issue 15 , 2015 , Pages 2608-2630 ; 10498923 (ISSN)
  9. URL: http://onlinelibrary.wiley.com/doi/10.1002/rnc.3215/abstract