Research on dynamic modeling and performance analysis of helicopter turboshaft engine's start-up process

Author:

Sheng Hanlin,Chen Qian,Li Jiacheng,Jiang Wei,Wang Zhe,Liu Ziwen,Zhang Tianhong,Liu Yuan

Funder

National Natural Science Foundation of China

Aviation Science Foundation of China

Aeronautics Power Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Design and implementation of MPC for turbofan engine control system;Montazeri-Gh;Aerosp. Sci. Technol.,2019

2. A novel distributed extended Kalman filter for aircraft engine gas-path health estimation with sensor fusion uncertainty;Lu;Aerosp. Sci. Technol.,2019

3. Robust tracking control of aero-engine rotor speed based on switched LPV model;Liu;Aerosp. Sci. Technol.,2019

4. Simulation of Turbofan Engine;Mc Kinney,1967

5. TURBOTRANS-A Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems;Palmer,1982

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