Integrated design and control of hypersonic vehicles

Srikanth Sridharan; Justin A. Echols; Armando Rodriguez; Kaustav Mondal

doi:10.1109/ACC.2014.6859438

Integrated design and control of hypersonic vehicles

Srikanth Sridharan, Justin A. Echols, Armando Rodriguez, Kaustav Mondal

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

16 Scopus citations

Abstract

In this paper we consider the design and control of an airbreathing hypersonic vehicle. Such vehicles are characterized by non-minimum phase characteristics, instability, actuator saturation constraints, and lightly damped flexible modes.While traditional vehicle design has followed an iterative sequential procedure (with the controller design following an aero-centric vehicle design phase), an integrated vehicle-control design process (based on bilinear matrix inequalities) is considered in this paper. We consider several example problems to illustrate the advantages of such an approach.

Original language	English (US)
Title of host publication	2014 American Control Conference, ACC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1371-1376
Number of pages	6
ISBN (Print)	9781479932726
DOIs	https://doi.org/10.1109/ACC.2014.6859438
State	Published - Jan 1 2014
Event	2014 American Control Conference, ACC 2014 - Portland, OR, United States Duration: Jun 4 2014 → Jun 6 2014

Publication series

Name	Proceedings of the American Control Conference
ISSN (Print)	0743-1619

Other

Other	2014 American Control Conference, ACC 2014
Country/Territory	United States
City	Portland, OR
Period	6/4/14 → 6/6/14

Keywords

Aerospace
Optimization
Robust control

ASJC Scopus subject areas

Electrical and Electronic Engineering

Access to Document

10.1109/ACC.2014.6859438

Cite this

Integrated design and control of hypersonic vehicles. / Sridharan, Srikanth; Echols, Justin A.; Rodriguez, Armando et al.
2014 American Control Conference, ACC 2014. Institute of Electrical and Electronics Engineers Inc., 2014. p. 1371-1376 6859438 (Proceedings of the American Control Conference).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Sridharan, S, Echols, JA, Rodriguez, A & Mondal, K 2014, Integrated design and control of hypersonic vehicles. in 2014 American Control Conference, ACC 2014., 6859438, Proceedings of the American Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 1371-1376, 2014 American Control Conference, ACC 2014, Portland, OR, United States, 6/4/14. https://doi.org/10.1109/ACC.2014.6859438

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AB - In this paper we consider the design and control of an airbreathing hypersonic vehicle. Such vehicles are characterized by non-minimum phase characteristics, instability, actuator saturation constraints, and lightly damped flexible modes.While traditional vehicle design has followed an iterative sequential procedure (with the controller design following an aero-centric vehicle design phase), an integrated vehicle-control design process (based on bilinear matrix inequalities) is considered in this paper. We consider several example problems to illustrate the advantages of such an approach.

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Integrated design and control of hypersonic vehicles

Abstract

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Keywords

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