Engine control design using compressor guided vanes during autorotation power recovery

DOI10.1007/s13369-016-2336-7zbMath1390.93340OpenAlexW2540692825MaRDI QIDQ1640463

Fengyong Sun, Hai-Bo Zhang

Publication date: 14 June 2018

Published in: Arabian Journal for Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s13369-016-2336-7

zbMATH Keywords

controlhelicopterintegrated modelautorotationengine

Mathematics Subject Classification ID

(H^infty)-control (93B36) Pole and zero placement problems (93B55) Analytic circuit theory (94C05)

Related Items (3)

Event-triggered fault-tolerant control for input-constrained nonlinear systems with mismatched disturbances via adaptive dynamic programming ⋮ Predictor-based optimal robust guaranteed cost control for uncertain nonlinear systems with completely tracking errors constraint ⋮ Adaptive fuzzy hierarchical sliding mode control of uncertain under-actuated switched nonlinear systems with actuator faults

Cites Work

• Unnamed Item
• Robust full degree-of-freedom tracking control of a helicopter
• Analytical prediction of height-velocity diagram of a helicopter using optimal control theory
• H/sub ∞/ design with pole placement constraints: an LMI approach
• Robust Exact Pole Placement via an LMI-Based Algorithm

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