Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle
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 prac...
Saved in:
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2010-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2010/474537 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832565194907189248 |
|---|---|
| author | M. Bahrami B. Ebrahimi G. R. Ansarifar |
| author_facet | M. Bahrami B. Ebrahimi G. R. Ansarifar |
| author_sort | M. Bahrami |
| collection | DOAJ |
| description | 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. |
| format | Article |
| id | doaj-art-b8dd5008636f4be59378ee9fdcc52e7a |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2010-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-b8dd5008636f4be59378ee9fdcc52e7a2025-02-03T01:09:11ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742010-01-01201010.1155/2010/474537474537Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight VehicleM. Bahrami0B. Ebrahimi1G. R. Ansarifar2Department of Mechanical Engineering, Amirkabir University of Technology, Tehran, IranAerospace Research Institute, Ministry of Science Research and Technology, Tehran, IranDepartment of Mechanical Engineering, Amirkabir University of Technology, Tehran, IranDesign 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.http://dx.doi.org/10.1155/2010/474537 |
| spellingShingle | M. Bahrami B. Ebrahimi G. R. Ansarifar Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle International Journal of Aerospace Engineering |
| title | Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle |
| title_full | Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle |
| title_fullStr | Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle |
| title_full_unstemmed | Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle |
| title_short | Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle |
| title_sort | sliding mode observer and control design with adaptive parameter estimation for a supersonic flight vehicle |
| url | http://dx.doi.org/10.1155/2010/474537 |
| work_keys_str_mv | AT mbahrami slidingmodeobserverandcontroldesignwithadaptiveparameterestimationforasupersonicflightvehicle AT bebrahimi slidingmodeobserverandcontroldesignwithadaptiveparameterestimationforasupersonicflightvehicle AT gransarifar slidingmodeobserverandcontroldesignwithadaptiveparameterestimationforasupersonicflightvehicle |