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The air extraction control system of high-altitude cabin coordinates the control of multiple valves to connect the compressor units to the extraction pipeline network and establish the environmental back pressure of the engine to simulate the flight altitude for engine testing. This paper proposes a collaborative optimization control scheme and algorithm based on an internal penalty function to address issues such as low efficiency during the connection of multiple compressor units,potential exceeding of safety margins in compressor unit pressure ratio,and poor pressure control quality in the extraction pipeline network. Firstly,a safety constraint pressure optimization framework was established using an internal penalty function to ensure the safety operation of grid-connection of compressor units. Secondly,a collaborative optimization control algorithm was designed by integrating active disturbance rejection control(ADRC)and PI control to improve connection efficiency and pressure control quality. Multiple practical working conditions were simulated to verify the proposed scheme and algorithm. The results demonstrate that compared to the currently employed independent control,the proposed algorithm can improve system grid-connection efficiency and control quality while ensuring the safety of units. Under the condition of sudden increase and decrease in engine exhaust flow,the time to reach the set pressure was shortened by 16.5%,the maximum instantaneous pressure fluctuations caused by sudden flow increase and decrease were reduced by 13.4% and 15.5% respectively,the adjustment time was shortened by 56%,the control was stable without overshoot and the swing range of the core control valve was decreased from 5% to 0.32%. © 2025 China Aerospace Science and Industry Corp. All rights reserved.
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Journal of Propulsion Technology
ISSN: 1001-4055
Year: 2025
Issue: 7
Volume: 46
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ESI Highly Cited Papers on the List: 0 Unfold All
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30 Days PV: 0
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