Switching control of thrust regulation and inlet unstart protection for scramjet engine based on strategy of integral initial values resetting

Cao, Ruifeng; Chang, Juntao; Tang, Jingfeng; Bao, Wen; Yu, Daren; Wang, Zhongqi

doi:10.1016/j.ast.2015.06.023

Cited by 12 publications

(5 citation statements)

References 27 publications

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“…In other words, it is not a global optimal solution for the engine control problem also extended their proposal based on the strategy of integral initial values resetting in 2015. 152 In 2018, Zheng et al published ''Performance uncertainty propagation analysis for controloriented model of a turbine-based combined cycle engine'' and investigated on the source of these uncertainties, performed model simulation with uncertainties inputs and finally gave a full analysis for their control model to confirm the effectiveness of the proposed approach in realworld control scenarios. 153 In 2018, Ma et al presented a control-oriented modeling approach used in a real-time simulation platform for a dual-mode scramjet combustor.…”

Section: Control Algorithm Phases Advantages Disadvantagesmentioning

confidence: 99%

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A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion

Mohammadi

Fashandi

Jafari

et al. 2020

Measurement and Control

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The gas turbine aero-engine control systems over the past eight decades have been thoroughly investigated. This review purposes are to present a comprehensive reference for aero-engine control design and development based on a systematic scientometric analysis and to categorize different methods, algorithms, and approaches taken into account to improve the performance and operability of aircraft engines from the first days to present to enable this challenging technology to be adopted by aero-engine manufacturers. Initially, the benefits of the control systems are restated in terms of improved engine efficiency, reduced carbon dioxide emissions, and improved fuel economy. This is followed by a historical coverage of the proposed concepts dating back to 1936. A comprehensive scientometric analysis is then presented to introduce the main milestones in aero-engines control. Possible control strategies and concepts are classified into four distinct phases, including Single input- single output control algorithms, MIN-MAX or Cascade control algorithms, advanced control algorithms, More-electric and electronic control algorithms and critically reviewed. The advantages and disadvantages of milestones are discussed to cover all practical aspects of the review to enable the researchers to identify the current challenges in aircraft engine control systems.

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Section: Control Algorithm Phases Advantages Disadvantagesmentioning

confidence: 99%

“…151 They also extended their proposal based on the strategy of integral initial values resetting in 2015. 152…”

Section: A Historical Review Of Gas Turbine Engine Controlmentioning

confidence: 99%

A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion

Mohammadi

Fashandi

Jafari

et al. 2020

Measurement and Control

View full text Add to dashboard Cite

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“…However, many traditional measures to handle output constraints sacrifice speed performance to guarantee safety. An effective strategy to deal with the contradiction between rapidity performance and safety requirements is to apply a switching control scheme . Under the switching multi‐objective control scheme, controllers for respective objectives are designed separately without consideration of other constraints.…”

Section: Introductionmentioning

confidence: 99%

“…The aero-engine is the most essential driven section of the aero-craft and therefore has attracted significant attention from researchers in recent years [1][2][3][4][5]. There are various engine safety boundaries during aero-craft operations.…”

Section: Introductionmentioning

confidence: 99%

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Switching Control of Acceleration and Safety Protection for Turbo Fan Aero‐Engines Based on Equilibrium Manifold Expansion Model

Chen

Zhao

2018

Asian Journal of Control

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This paper presents a switching control strategy to solve the acceleration problem with safety constraints for aero‐engines. The proposed strategy is based on an equilibrium manifold expansion (EME) model. That brings a more precise description for the dynamic behavior of the aero‐engine during the acceleration procedure. The acceleration controller, the safety protection controller, and the set‐point controller are designed separately for the respective objectives with more degree of freedom and less conservatism. Based on Lyapunov function, the switching law is properly designed to ensure asymptotic stability with acceleration constraint and the high pressure turbine outlet temperature safety constraint for the nonlinear EME model. It is not necessary to construct a minimum phase nonlinear system using the proposed strategy. The effectiveness of the proposed strategy is verified through a case study where the controller designed based on the EME model is used for a nonlinear component‐level (NCL) model. Simulation also indicates better performance from using the proposed strategy than the existing method.

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Multi-objective coordinated control of regeneratively-cooled scramjet engine with two-stage kerosene injection

Jun-hai

Chang

Huang

et al. 2019

Aerospace Science and Technology

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Switching control of thrust regulation and inlet unstart protection for scramjet engine based on strategy of integral initial values resetting

Cited by 12 publications

References 27 publications

A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion

A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion

Switching Control of Acceleration and Safety Protection for Turbo Fan Aero‐Engines Based on Equilibrium Manifold Expansion Model

Multi-objective coordinated control of regeneratively-cooled scramjet engine with two-stage kerosene injection

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