![](/images/graphics-bg.png)
Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle
Joint Authors
Bahrami, M.
Ansarifar, G. R.
Ebrahimi, B.
Source
International Journal of Aerospace Engineering
Issue
Vol. 2010, Issue 2010 (31 Dec. 2010), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2010-06-28
Country of Publication
Egypt
No. of Pages
9
Main Subjects
Engineering Sciences and Information Technology
Abstract EN
Design and synthesis of a nonlinear generic supersonic flight vehicle longitudinal dynamics control for angle-of-attack, AOA, output tracking in the atmospheric flight is presented based on sliding mode control.
A sliding mode observer is invoked to estimate AOA which is difficult to measure in practice.
Large parameter uncertainties accommodation envisaged by designing adaptive mechanisms for both the control and observer and high chattering authority due to large deviations of aerodynamic coefficients arising from wind-tunnel measurements are inhibited.
The employed method enables the sliding mode control design to exhibit the desired dynamic properties during the entire output-tracking process.
Simulations results are presented to demonstrate the performance, robustness, and stability.
American Psychological Association (APA)
Bahrami, M.& Ebrahimi, B.& Ansarifar, G. R.. 2010. Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle. International Journal of Aerospace Engineering،Vol. 2010, no. 2010, pp.1-9.
https://search.emarefa.net/detail/BIM-474434
Modern Language Association (MLA)
Bahrami, M.…[et al.]. Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle. International Journal of Aerospace Engineering No. 2010 (2010), pp.1-9.
https://search.emarefa.net/detail/BIM-474434
American Medical Association (AMA)
Bahrami, M.& Ebrahimi, B.& Ansarifar, G. R.. Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle. International Journal of Aerospace Engineering. 2010. Vol. 2010, no. 2010, pp.1-9.
https://search.emarefa.net/detail/BIM-474434
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-474434