A novel emergent state control law for an integrated helicopter/turboshaft engine system

DOI10.1155/2014/385807zbMath1407.93302OpenAlexW2058344209WikidataQ59064885 ScholiaQ59064885MaRDI QIDQ1718241

Xianqiang Yang

Publication date: 8 February 2019

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2014/385807

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Application models in control theory (93C95)

Cites Work

• Unnamed Item
• Continuous-time analysis, eigenstructure assignment, and H/sub 2/ synthesis with enhanced linear matrix inequalities (LMI) characterizations
• Solving Rank-Constrained LMI Problems With Application to Reduced-Order Output Feedback Stabilization

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