TY - GEN
T1 - Physics Informed Data Fusion Model for Uncertainty Quantification in Atmospheric Entry Vehicle Dynamic Stability
AU - Shafi Al, Shafi Al Salman
AU - Oz, Furkan
AU - Kassem, Ashraf
AU - San, Omer
AU - Kara, Kursat
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - This paper presents an advanced methodology for enhancing the accuracy of trajectory prediction of atmospheric entry vehicles by combining experimental and numerically simulated data. The study utilizes sparse oscillation observation from the ballistic range during the deceleration phase of entry vehicles. It aims to enhance the accuracy of predictions by integrating these ballistic range observations with available free-flight computational fluid dynamics (FF-CFD) data. The proposed method consists of two main components. First, Bayesian optimization-based Gaussian processes seamlessly combine the ballistic range and FF-CFD datasets. Second, the proposed method utilizes the equations of motion to refine prediction accuracy and uncertainty further. This is achieved through a Physics-Informed Gaussian Neural Network (PI-GNN), which interfaces with the system’s governing differential equation to optimize dynamic stability, leading to a more robust understanding of the vehicle’s landing. This integrated approach represents a novel strategy for uncertainty quantification in atmospheric entry vehicle dynamics, enhancing the reliability and precision of predictive models.
AB - This paper presents an advanced methodology for enhancing the accuracy of trajectory prediction of atmospheric entry vehicles by combining experimental and numerically simulated data. The study utilizes sparse oscillation observation from the ballistic range during the deceleration phase of entry vehicles. It aims to enhance the accuracy of predictions by integrating these ballistic range observations with available free-flight computational fluid dynamics (FF-CFD) data. The proposed method consists of two main components. First, Bayesian optimization-based Gaussian processes seamlessly combine the ballistic range and FF-CFD datasets. Second, the proposed method utilizes the equations of motion to refine prediction accuracy and uncertainty further. This is achieved through a Physics-Informed Gaussian Neural Network (PI-GNN), which interfaces with the system’s governing differential equation to optimize dynamic stability, leading to a more robust understanding of the vehicle’s landing. This integrated approach represents a novel strategy for uncertainty quantification in atmospheric entry vehicle dynamics, enhancing the reliability and precision of predictive models.
UR - http://www.scopus.com/inward/record.url?scp=85203690703&partnerID=8YFLogxK
U2 - 10.2514/6.2024-4446
DO - 10.2514/6.2024-4446
M3 - Conference contribution
AN - SCOPUS:85203690703
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation Forum and ASCEND, 2024
Y2 - 29 July 2024 through 2 August 2024
ER -