Control law synthetizing for an innovative indirect precooled airbreathing engine under off-design operation conditions
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DOI: 10.1016/j.energy.2022.126110
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References listed on IDEAS
- Yu, Xuanfei & Wang, Cong & Yu, Daren, 2020. "Series view method based thermodynamic modeling and analysis for innovative precooled aeroengines with different turbine-compressor coupling schemes," Energy, Elsevier, vol. 205(C).
- Yu, Xuanfei & Pan, Xin & Zheng, Jialin & Wang, Cong & Yu, Daren, 2017. "Thermodynamic spectrum of direct precooled airbreathing propulsion," Energy, Elsevier, vol. 135(C), pages 777-787.
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- Lv, Chengkun & Huang, Qian & Wang, Ziao & Chang, Juntao & Yu, Daren, 2024. "Mode transition control law analysis of ammonia MIPCC aeroengine considering inlet–compressor safety matching," Energy, Elsevier, vol. 288(C).
- Wen, Jie & Wan, Chenxi & Xu, Guoqiang & Zhuang, Laihe & Dong, Bensi & Chen, Junjie, 2024. "Optimization of thermal management system architecture in hydrogen engine employing improved genetic algorithm," Energy, Elsevier, vol. 297(C).
- Lv, Chengkun & Lan, Zhu & Wang, Ziao & Chang, Juntao & Yu, Daren, 2024. "Intelligent ammonia precooling control for TBCC mode transition based on neural network improved equilibrium manifold expansion model," Energy, Elsevier, vol. 288(C).
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Keywords
Engine control; Off-design modeling; Propulsion; Single stage to orbit; Trajectory;All these keywords.
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