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Montazeri, M., Foroozannejad, M., Yousefi Dastjerdi, A., Bordbar, A. (2025). Integrated Simulation and Control of Turbojet Engine Dynamics and Fixed-wing Airplane Flight Dynamics. Electronic and Cyber Defense, 20(4), 103-116.
Morteza Montazeri; Mahdi Foroozannejad; Ali Yousefi Dastjerdi; Abdollah Bordbar. "Integrated Simulation and Control of Turbojet Engine Dynamics and Fixed-wing Airplane Flight Dynamics". Electronic and Cyber Defense, 20, 4, 2025, 103-116.
Montazeri, M., Foroozannejad, M., Yousefi Dastjerdi, A., Bordbar, A. (2025). 'Integrated Simulation and Control of Turbojet Engine Dynamics and Fixed-wing Airplane Flight Dynamics', Electronic and Cyber Defense, 20(4), pp. 103-116.
Montazeri, M., Foroozannejad, M., Yousefi Dastjerdi, A., Bordbar, A. Integrated Simulation and Control of Turbojet Engine Dynamics and Fixed-wing Airplane Flight Dynamics. Electronic and Cyber Defense, 2025; 20(4): 103-116.

Integrated Simulation and Control of Turbojet Engine Dynamics and Fixed-wing Airplane Flight Dynamics

مکانیک هوافضا
Article 7, Volume 20, Issue 4 - Serial Number 78, March 2025, Pages 103-116    PDF (1.04 M)
Document Type: Dynamics, Vibrations, and Control
Authors
Morteza Montazeri* 1; Mahdi Foroozannejad2; Ali Yousefi Dastjerdi2; Abdollah Bordbar2
1Corresponding author: Professor, Faculty of Mechanical Engineering, Iran University of Science and Technology, Tehran, Iran
2Ph.D. Student, Faculty of Mechanical Engineering, Iran University of Science and Technology, Tehran, Iran
Receive Date: 28 September 2024,  Revise Date: 05 November 2024,  Accept Date: 17 November 2024 
Abstract
In this article, the simulation and integrated control of flight-propulsion are addressed as a significant and necessary research topic in the aerospace industry. In previous research, flight control and turbine engine control have often been treated separately; however, the mutual effects of flight dynamics and turbine engine dynamics on one another have received less attention. Initially, to model the movement of the UAV body, kinematic and flight dynamics equations are presented. Transmission equations are developed based on Newton’s laws, and rotational equations are derived from Euler’s theory. Subsequently, the thermodynamic and dynamic equations necessary for turbojet engine modeling are introduced. The equations governing the engine inlet opening, compressor, turbine, combustion chamber, and nozzle are examined separately. All simulations are conducted in MATLAB/Simulink. Flight graphic is displayed in real-time using FlightGear software. A structure for simulating and controlling flight dynamics and engine dynamics is proposed, addressing not only the control of flight and the UAV’s trajectory but also the control of the shaft’s rotational speed while observing the limitations of the turbojet engine. Additionally, flight-propulsion control coefficients are simultaneously optimized for a specific mission using genetic algorithm. Finally, the simulation results are presented and discussed.

Highlights
  • Optimization of control coefficients
  • Interactions between flight dynamics and turbojet engine dynamics
  • Real-time flight display
  • Desired speed and height tracking with respect to engine limitations
Keywords
Integrated flight-propulsion control; Min-max fuel controller; Thermodynamic model of turbojet; Genetic algorithm; Fixed wing UAV flight dynamics
References

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