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

Jun-hai, MA; Chang, Juntao; Huang, QingPing; Bao, Wen; Yu, Daren

doi:10.1016/j.ast.2019.04.027

Cited by 14 publications

(3 citation statements)

References 42 publications

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“…154 They also extended their study to unsteady one-dimensional feature for a hydrocarbon regeneratively-cooled scramjet engine 155 and multi-objective coordinated control of a regeneratively-cooled scramjet engine with twostage kerosene injection. 156 In 2019, Zheng et al published a study titled ''Modeling and analysis for integrated airframe/ propulsion control of vehicles during mode transition of over-under Turbine-Based-Combined-Cycle engines.'' They described mode transition control as a critical issue of the Turbine-Based-Combined Cycle (TBCC) engine and proposed a nonlinear longitudinal TBCC-powered dynamic vehicle model and designed a control-oriented model with six control inputs which were obtained by approximately expressing aerodynamic coefficients through curve-fitting methods.…”

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%

Section: More Electric and Electronic Control Algorithms Since 2004mentioning

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

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“…In order to develop the sustainable decision support system for the FRP, the development of a smart and environmentally friendly new rescheduling methodology is considered essential to maintain the sustainable development of air transport. Within this framework, the adoption of a new rescheduling methodology should be reducing the harmful effects of pollution as much as possible and improving the flow of air traffic [15,16].…”

Section: Introductionmentioning

confidence: 99%

Optimization of Flight Rescheduling Problem under Carbon Tax

2020

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The flight rescheduling problem is one of the major challenges of air traffic issue. Unforeseen bad weather conditions stimulate air traffic congestion and make the initial scheduling infeasible, resulting in significant economic losses for passengers and airlines. Furthermore, due to rigorous environmental legislations, flight rescheduling becomes a more complicated problem, as it has to deal with flight delays on the one hand, and carbon emissions on the other hand. In this paper, we address the flight rescheduling problem with an environmental requirement subject to the air capacity limitation due to bad weather conditions. A new strategy is proposed to minimize the disruption effects on planned flights, which adopted ground delay, longer route change, flight cancellation, as well speed adjustment to arrive at a scheduled time. Firstly, the objective of this study is to determine the economical flights plan in line with the new available air capacity. Secondly, by considering the environmental impact of the kerosene consumption, we illustrate the contribution of an economical decision to aircraft emissions. Experiment results are provided to show the efficiency of the proposed strategies and genetic algorithm as the used optimization method. Furthermore, the impacts of carbon tax and cost of arrival delay on the flights carbon emissions are studied.

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Prediction model of temperature field in dual-mode combustors based on wall pressure

Kong

Quan

et al. 2022

Acta Astronautica

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

Cited by 14 publications

References 42 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

Optimization of Flight Rescheduling Problem under Carbon Tax

Prediction model of temperature field in dual-mode combustors based on wall pressure

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