Robust fault detection for a jet engine using robust l 1 Estimation 1

Curry, T.; Collins, Emmanuel G.

doi:10.1016/s1474-6670(17)36487-x

Cited by 1 publication

(2 citation statements)

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“…Many of the project accomplishments are well documented in several publications [1][2][3][4][5][6][7][8]. Hence, this section briefly summarizes the main results and refers to the appropriate publications.…”

Section: Project Accomplishmentsmentioning

confidence: 99%

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Feedback Control Design for Counterflow Thrust Vectoring

Collins¹,

Emmanuel²

2005

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The public reporting burden for this collection of information is estimated to average 1 hour per response, including SUPPLEMENTARY NOTES ABSTRACTEngineering research over the last few years has successfully demonstrated the potential of thrust vector control using counterflow at conditions up to Mach 2. Before this study, research had been limited to open-loop studies of counterflow thrust vectoring. For practical implementation it was vital that the counterflow scheme be used in conjunction with feedback control. Hence, the focus of this research was to develop and experimentally demonstrate a feedback control design methodology for counterflow thrust vectoring. This research focused on 2-D (pitch) thrust vectoring. The main goal was the design and implementation of robust controllers that yield closed-loop systems with fast response times, and avoid overshoot in order to aid in the avoidance of attachment. Additionally, these controllers should be simple and easy to implement and the methodology used to design them should be valid for the more difficult case of 3-D thrust vectoring, which leads to multiple-input, multiple-output control problems.

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Section: Project Accomplishmentsmentioning

confidence: 99%

“…This approach to FDI was successfully demonstrated using a linearized model of a jet engine and was also applied to a complex, nonlinear benchmark problem. The results of this research were published in [1,3,7,8] …”

Section: Feedback Control For Counterflow Thrust Vectoring With a Turmentioning

confidence: 99%

Feedback Control Design for Counterflow Thrust Vectoring

Collins¹,

Emmanuel²

2005

View full text Add to dashboard Cite

show abstract

Robust fault detection for a jet engine using robust l 1 Estimation 1

Cited by 1 publication

References 15 publications

Feedback Control Design for Counterflow Thrust Vectoring

Feedback Control Design for Counterflow Thrust Vectoring

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