| Citation: | LI Wentao, YU Duokui, PANG Haoyu, et al. Cooperative control of aero-engine binary vector nozzle[J]. Journal of Aerospace Power, 2026, 41（2）：20240819 doi: 10.13224/j.cnki.jasp.20240819
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In order to solve the problems of synergism that have not been considered in the control process of aero-engine binary vector nozzle and some safety performance indexes that cannot be met, a scheme for the cooperative control of aero-engine binary vector nozzle was proposed based on forward and inverse models. Meanwhile, a dynamic command planning algorithm and a fuzzy event-triggered cooperative control algorithm were developed. The dynamic control performance of the binary vector nozzle under various conditions was verified. Simulation results showed that the cooperative scheme eliminated the anti-regulation issue of the nozzle exit area, and the dynamic tracking accuracy of the ratio of the exit area to the throat area was controlled within 5%, presenting great significance for the safe control of the aero-engine.
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