作者: Richard P. Meisner , Gi Yun Chung , Manuj Dhingra , Jonnalagadda V. R. Prasad
DOI:
关键词: Operating point 、 Component (UML) 、 Partial derivative 、 Gas turbines 、 Function (mathematics) 、 Linearization 、 Engineering 、 Control theory 、 Control engineering 、 Model based control
摘要: A method for model-based control of a gas turbine engine is disclosed. An operating point the generated from measured parameters using component-level model. The model analytically linearized by taking first partial derivative output each component with respect to input component, and evaluating result at point. Components are combined form perturbational engine, which inverted solve commands as function target parameters.