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Gas Path Fault Tolerant Control of Aero-Engine Based on On-Board Model
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作者 WANG Cancan LI Zhengxin HUANG Jinquan 《Aerospace China》 2021年第4期48-54,共7页
A fault tolerant control method is proposed in this paper for a turbofan engine gas path degradation through the full flight envelope. A Quantum-behaved Particle Swarm Optimization(QPSO) algorithm is applied to obtain... A fault tolerant control method is proposed in this paper for a turbofan engine gas path degradation through the full flight envelope. A Quantum-behaved Particle Swarm Optimization(QPSO) algorithm is applied to obtain engine inputs adjustments, which contribute to construct off-line performance accommodation interpolation schedules. With a double closed-loop control system structure, command control is corrected based on real-time fault diagnostic results. Simulations indicate that fault tolerant control could reduce thrust and stall margin loss effectively in gas path faults. 展开更多
关键词 AERO-ENGINE gas path fault fault tolerant control QPSO algorithm
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