Application of LPV modeling, design and analysis methods to a re-entry vehicle

A. Marcos; J. Veenman; C.W. Scherer; G. De Zaiacomo; D. Mostaza; M. Kerr; H. Koroglu; S. Bennani

Application of LPV modeling, design and analysis methods to a re-entry vehicle

A. Marcos, J. Veenman, C.W. Scherer, G. De Zaiacomo, D. Mostaza, M. Kerr, H. Koroglu, S. Bennani

Control Systems

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

Abstract

In this paper the application of linear parameter varying (LPV) modeling, design and analysis methods to a re-entry vehicle is presented The selected atmospheric re-entry benchmaik includes full nonlinear motion, a detailed aerodynamic database (from hypersonic to subsonic), relevant actuator and sensor models and physically-meaningful aerodynamic and parametric uncertainty profiles The results show that (i) LPV controller design methods can solve gain-scheduling problems in a very effective manner, (ii) integral quadratic constraint (IQC) analysis methods can be used very efficiently to accurately interpret the nonlinear time domain simulation results, and, (iii) the use of linear fractional transfoi mation (LFT) and LPV modeling representations are key to a successful analysis

Original language	English
Title of host publication	Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada
Place of Publication	Washington
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	8192-1/18
Publication status	Published - 2010

Cite this

Marcos, A., Veenman, J., Scherer, C. W., De Zaiacomo, G., Mostaza, D., Kerr, M., Koroglu, H., & Bennani, S. (2010). Application of LPV modeling, design and analysis methods to a re-entry vehicle. In Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada (pp. 8192-1/18). American Institute of Aeronautics and Astronautics Inc. (AIAA).

@inproceedings{2aecb0abcf554515b9bd0798cd102368,

title = "Application of LPV modeling, design and analysis methods to a re-entry vehicle",

abstract = "In this paper the application of linear parameter varying (LPV) modeling, design and analysis methods to a re-entry vehicle is presented The selected atmospheric re-entry benchmaik includes full nonlinear motion, a detailed aerodynamic database (from hypersonic to subsonic), relevant actuator and sensor models and physically-meaningful aerodynamic and parametric uncertainty profiles The results show that (i) LPV controller design methods can solve gain-scheduling problems in a very effective manner, (ii) integral quadratic constraint (IQC) analysis methods can be used very efficiently to accurately interpret the nonlinear time domain simulation results, and, (iii) the use of linear fractional transfoi mation (LFT) and LPV modeling representations are key to a successful analysis",

author = "A. Marcos and J. Veenman and C.W. Scherer and {De Zaiacomo}, G. and D. Mostaza and M. Kerr and H. Koroglu and S. Bennani",

year = "2010",

language = "English",

pages = "8192--1/18",

booktitle = "Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

address = "United States",

}

Marcos, A, Veenman, J, Scherer, CW, De Zaiacomo, G, Mostaza, D, Kerr, M, Koroglu, H & Bennani, S 2010, Application of LPV modeling, design and analysis methods to a re-entry vehicle. in Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada. American Institute of Aeronautics and Astronautics Inc. (AIAA), Washington, pp. 8192-1/18.

Application of LPV modeling, design and analysis methods to a re-entry vehicle. / Marcos, A.; Veenman, J.; Scherer, C.W. et al.
Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada. Washington: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2010. p. 8192-1/18.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

TY - GEN

T1 - Application of LPV modeling, design and analysis methods to a re-entry vehicle

AU - Marcos, A.

AU - Veenman, J.

AU - Scherer, C.W.

AU - De Zaiacomo, G.

AU - Mostaza, D.

AU - Kerr, M.

AU - Koroglu, H.

AU - Bennani, S.

PY - 2010

Y1 - 2010

N2 - In this paper the application of linear parameter varying (LPV) modeling, design and analysis methods to a re-entry vehicle is presented The selected atmospheric re-entry benchmaik includes full nonlinear motion, a detailed aerodynamic database (from hypersonic to subsonic), relevant actuator and sensor models and physically-meaningful aerodynamic and parametric uncertainty profiles The results show that (i) LPV controller design methods can solve gain-scheduling problems in a very effective manner, (ii) integral quadratic constraint (IQC) analysis methods can be used very efficiently to accurately interpret the nonlinear time domain simulation results, and, (iii) the use of linear fractional transfoi mation (LFT) and LPV modeling representations are key to a successful analysis

AB - In this paper the application of linear parameter varying (LPV) modeling, design and analysis methods to a re-entry vehicle is presented The selected atmospheric re-entry benchmaik includes full nonlinear motion, a detailed aerodynamic database (from hypersonic to subsonic), relevant actuator and sensor models and physically-meaningful aerodynamic and parametric uncertainty profiles The results show that (i) LPV controller design methods can solve gain-scheduling problems in a very effective manner, (ii) integral quadratic constraint (IQC) analysis methods can be used very efficiently to accurately interpret the nonlinear time domain simulation results, and, (iii) the use of linear fractional transfoi mation (LFT) and LPV modeling representations are key to a successful analysis

M3 - Conference contribution

SP - 8192-1/18

BT - Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

CY - Washington

ER -

Application of LPV modeling, design and analysis methods to a re-entry vehicle

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