Related Experiment Video
Updated: Jun 20, 2025

04:58
A Rapid Method for Modeling a Variable Cycle Engine
Published on: August 13, 2019
7.5K
Aircraft turnaround time dynamic prediction based on Time Transition Petri Net
Yanyu Cui1, Linyan Ma2, Qingmiao Ding1
1College of Aeronautical Engineering, Civil Aviation University of China, Tianjin, China.
Plos One
|July 18, 2024
Summary
Accurate aircraft turnaround time prediction is crucial for airport efficiency. This study proposes a novel Bayesian method using Time Transition Petri Nets, achieving high accuracy for predicting flight turnaround times.
Area of Science:
- Operations Research
- Aerospace Engineering
Background:
- Efficient airport operations rely on accurate aircraft turnaround time prediction.
- Coordinating ground services is essential for improving overall airport efficiency.
Purpose of the Study:
- To develop a dynamic prediction method for aircraft turnaround time.
- To improve flight punctuality and airport clearance levels through accurate predictions.
Main Methods:
- Analysis of the aircraft turnaround operation process.
- Development of a Time Transition Petri Net (TTPN) model to describe operations.
- Design of a dynamic turnaround time prediction method using Bayesian theorem and historical flight data.
- Application of Shapiro-Wilke test for prior probability distribution validation.
Main Results:
- The proposed TTPN model effectively describes the flight turnaround process and operational logic.
- The Bayesian prediction method, utilizing actual landing times, demonstrated strong performance.
- Validation against real-world data from a major Chinese airport yielded a root-mean-square error of 3.75 minutes and a mean absolute error of 3.40 minutes.
Conclusions:
- The developed method provides accurate aircraft turnaround time predictions.
- This approach contributes significantly to enhancing flight punctuality and airport operational efficiency.
- The integration of TTPN and Bayesian methods offers a robust solution for airport management.
Related Concept Videos
Time-Domain Interpretation of PD Control
87
Proportional-Derivative (PD) control is a widely used control method in various engineering systems to enhance stability and performance. In a system with only proportional control, common issues include high maximum overshoot and oscillation, observed in both the error signal and its rate of change. This behavior can be divided into three distinct phases: initial overshoot, subsequent undershoot, and gradual stabilization.
Consider the example of control of motor torque. Initially, a positive...
Consider the example of control of motor torque. Initially, a positive...
87
Multi-input and Multi-variable systems
105
Cruise control systems in cars are designed as multi-input systems to maintain a driver's desired speed while compensating for external disturbances such as changes in terrain. The block diagram for a cruise control system typically includes two main inputs: the desired speed set by the driver and any external disturbances, such as the incline of the road. By adjusting the engine throttle, the system maintains the vehicle's speed as close to the desired value as possible.
In the absence...
In the absence...
105
Multimachine Stability
150
Multimachine stability analysis is crucial for understanding the dynamics and stability of power systems with multiple synchronous machines. The objective is to solve the swing equations for a network of M machines connected to an N-bus power system.
In analyzing the system, the nodal equations represent the relationship between bus voltages, machine voltages, and machine currents. The nodal equation is given by:
In analyzing the system, the nodal equations represent the relationship between bus voltages, machine voltages, and machine currents. The nodal equation is given by:
150
Determination of Pi Terms
266
The Buckingham Pi theorem is a valuable method in dimensional analysis, reducing complex relationships between variables into dimensionless terms. Relevant variables in analyzing the lift force on an airplane wing include lift force, air density, wing area, aircraft velocity, and air viscosity. Expressing each variable in terms of fundamental dimensions — mass, length, and time — provides a consistent foundation for constructing these dimensionless terms.
The theorem indicates that...
The theorem indicates that...
266
Sequence Networks of Rotating Machines
98
A Y-connected synchronous generator, grounded through a neutral impedance, is designed to produce balanced internal phase voltages with only positive-sequence components. The generator's sequence networks include a source voltage that is exclusively in the positive-sequence network. The sequence components of line-to-ground voltages at the generator terminals illustrate this configuration.
Zero-sequence current induces a voltage drop across the generator's neutral impedance and other...
Zero-sequence current induces a voltage drop across the generator's neutral impedance and other...
98
Turbulent Flow: Problem Solving
109
Carbonation is a process used to dissolve carbon dioxide gas in a liquid, commonly used in the production of carbonated beverages. Achieving efficient carbonation requires careful control of temperature, pressure, and flow conditions. By adjusting these parameters, carbonation efficiency can be maximized, producing a higher concentration of CO2 in the liquid.
Temperature is a key factor in CO2 solubility. In this case, the CO2 gas and the liquid are cooled to 20°C. Lower temperatures...
Temperature is a key factor in CO2 solubility. In this case, the CO2 gas and the liquid are cooled to 20°C. Lower temperatures...
109

