Autopilot Design Method for the Blended Missile Based on Model Predictive Control
Joint Authors
Source
International Journal of Aerospace Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-13, 13 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-02-08
Country of Publication
Egypt
No. of Pages
13
Abstract EN
This paper develops a novel autopilot design method for blended missiles with aerodynamic control surfaces and lateral jets.
Firstly, the nonlinear model of blended missiles is reduced into a piecewise affine (PWA) model according to the aerodynamics properties.
Secondly, based on the equivalence between the PWA model and mixed logical dynamical (MLD) model, the MLD model of blended missiles is proposed taking into account the on-off constraints of lateral pulse jets.
Thirdly, a hybrid model predictive control (MPC) method is employed to design autopilot.
Finally, simulation results under different conditions are presented to show the effectiveness of the proposed method, which demonstrate that control allocation between aerodynamic control surfaces and lateral jets is realized by adjusting the weighting matrix in an index function.
American Psychological Association (APA)
Yang, Baoqing& Zhao, Yuyu. 2015. Autopilot Design Method for the Blended Missile Based on Model Predictive Control. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-13.
https://search.emarefa.net/detail/BIM-1064536
Modern Language Association (MLA)
Yang, Baoqing& Zhao, Yuyu. Autopilot Design Method for the Blended Missile Based on Model Predictive Control. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-13.
https://search.emarefa.net/detail/BIM-1064536
American Medical Association (AMA)
Yang, Baoqing& Zhao, Yuyu. Autopilot Design Method for the Blended Missile Based on Model Predictive Control. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-13.
https://search.emarefa.net/detail/BIM-1064536
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1064536