Research on Integrated Control Method for Helicopter/Turboshaft Engine with Variable Rotor Speed Based on the Error Between Engine Required and Real Output Torque

Author:

Wang Yong,Zheng Qiangang,Zhang Haibo,Chen Haoying

Funder

National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference21 articles.

1. Kalinin, D.V.: Multithreaded continuously variable transmission synthesis for next-generation helicopters. In: St.Petersburg: 29th Congress of International Council of the Aeronautical Science. September 7–12 (2014)

2. Reddinger, J.P.; Gandhi, F.; Kang, H.: Using control redundancy for power and vibration reduction on a compound helicopter at high speeds. J. Am. Helicopter Soc. 63(3), 1–13 (2018)

3. Kalinin, D.V.: Multithreaded continuously variable transmission synthesis for next-generation helicopters. In: St. Petersburg: 29th Congress of the International Council of the Aeronautical Sciences, pp. 7–12 (2014)

4. Snyder, C.A.; Acree Jr, C.W.: Preliminary assessment of variable speed power turbine technology on civil tiltrotor size and performance. In: TX: American Helicopter Society 68th Annual Forum, 1–3 May (2012)

5. DeSmidt, H.A.; Smith, E.C.; Bill, R.C.; Wang, K.-W.: Comprehensive modeling and analysis of rotorcraft variable speed propulsion system with coupled engine/transmission/rotor dynamics. NASA/CR-2013 -216502.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Research on Integrated Control Method of Coaxial High-Speed Helicopter/Engine Based on Power Prediction Feedforward;International Journal of Aeronautical and Space Sciences;2024-04-04

2. An Electromagnetic Torque Calibration Algorithm Based On Multiple Linear Regression Principle;2023 5th International Conference on Electrical Engineering and Control Technologies (CEECT);2023-12-15

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