A study on nonlinear model predictive control for helicopter/turboshaft engine with variable rotor speed based on piecewise objective function-Reference-Cited by-同舟云学术

A study on nonlinear model predictive control for helicopter/turboshaft engine with variable rotor speed based on piecewise objective function

Published:2020-09-16 Issue:4 Volume:23 Page:1671-1680
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian J Control

Author:

Wang Yong¹^ORCID,Peng Yerong¹,Xi Zhihua¹,Zhang Haibo¹

Affiliation:

1. College of Energy and Power Engineering Nanjing University of Aeronautics and Astronautics Nanjing China

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Fundamental Research Funds for the Central Universities

Publisher

Wiley

Subject

Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.2448

Reference19 articles.

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2. Using control redundancy for power and vibration reduction on a compound helicopter at high speeds[J];Reddinger J. P.;Journal of the American Helicopter Society,2018

3. SnyderC A AcreeJrC W.Preliminary assessment of variable speed power turbine technology on civil tiltrotor size and performance[C]. TX: American Helicopter Society 68th Annual Forum 1–3 May 2012.

4. DesSidtHA SmithEC BillRC WangKW.Comprehensive modeling and analysis of rotorcraft variable speed propulsion system with coupled engine/transmission/rotor dynamics [R].NASA/CR‐2013‐216502.

5. Possibilities and difficulties for rotorcraft using variable transmission drive trains