Zobrazeno 1 - 10
of 45
pro vyhledávání: '"Muxuan Pan"'
Publikováno v:
Aerospace, Vol 11, Iss 8, p 610 (2024)
This paper presents an integrated framework for aircraft engines, which consists of three phases: modeling, control, and experimental testing. The engine is formulated as an uncertain T–S fuzzy model. By a hierarchical dynamical parameter clusterin
Externí odkaz:
https://doaj.org/article/97ab028f5c234b20ae8dc0b7a99547f8
Publikováno v:
Aerospace, Vol 10, Iss 3, p 209 (2023)
Due to the strong representation ability and capability of learning from data measurements, deep reinforcement learning has emerged as a powerful control method, especially for nonlinear systems, such as the aero-engine control system. In this paper,
Externí odkaz:
https://doaj.org/article/bc0a48ead8024e6aa34241e9b492bd62
Publikováno v:
Aerospace, Vol 10, Iss 2, p 196 (2023)
The variable cycle engine switches working modes by way of changing variable-geometry components to achieve the dual advantages of high unit thrust and low specific fuel consumption. Due to the lack of a large amount of rig test data and the complex
Externí odkaz:
https://doaj.org/article/ed3de016b27142d0a0e8462b6896cac4
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
A novel estimation-based and dropout-dependent control design for distributed control systems of aeroengines with packet dropout is proposed. The packet dropout is described as an independent identically distributed (i.i.d.) Bernoulli process with kn
Externí odkaz:
https://doaj.org/article/442a67cbb8824ad49a8412fe0e6696f6
Publikováno v:
Aerospace, Vol 10, Iss 2, p 112 (2023)
The variable cycle engine selects the appropriate working mode through mode switch to meet the requirements of low specific fuel consumption and high unit thrust. When the variable cycle engine switches between different modes, it should ensure the s
Externí odkaz:
https://doaj.org/article/7041e407406f41928cb5c0102fc0fe17
Publikováno v:
Aerospace, Vol 9, Iss 8, p 442 (2022)
Accurate component maps, which can significantly affect the efficiency, reliability and availability of aero-engines, play a critical role in aero-engine performance simulation. Unfortunately, the information of component maps is insufficient, leadin
Externí odkaz:
https://doaj.org/article/ef776c076f154327813b4ef8d5197cca
Publikováno v:
IEEE Access, Vol 7, Pp 144813-144825 (2019)
This paper proposes a hierarchical multivariable robust control design for a class of uncertain nonlinear dynamic system. The dynamic system is described by an uncertain T-S fuzzy model. The uncertainties in the model are structure matched and norm-b
Externí odkaz:
https://doaj.org/article/6b5bb0a8af9245a6a36a162a62c7ffca
Publikováno v:
Applied Sciences, Vol 10, Iss 14, p 4929 (2020)
A robust output tracking controller is necessary for the safe and reliable operation of aeroengines. This paper aims at developing an H 2 / H ∞ output tracking approach for aeroengines. In order to improve the tracking performance of the traditiona
Externí odkaz:
https://doaj.org/article/d4c38a95bd9b48dba936b86456dce69a
Publikováno v:
Energies, Vol 12, Iss 19, p 3791 (2019)
Nonlinear component level model (NCLM) is a widely used model for aeroengines. However, it requires iterative calculation and is, therefore, time-consuming, which restricts its real-time application. This study aims at developing a simplified real-ti
Externí odkaz:
https://doaj.org/article/adcb7778c5d74b7fb2cb899a1c7f95b4
Publikováno v:
Energies, Vol 12, Iss 21, p 4043 (2019)
To accomplish the limit protection task, the Min-Max selection structure is generally adopted in current aircraft engine control strategies. However, since no relationship between controller switching and limit violation is established, this structur
Externí odkaz:
https://doaj.org/article/082c9fd314274b1a9e8845b481fac0da