TY - JOUR
T1 - Coupled Kernel Extreme Learning Machine and Cuckoo Search for Aerodynamic Modeling and Stability Analysis of Spinning Projectiles
AU - Liu, Qi
AU - Lei, Juanmian
N1 - Publisher Copyright:
© The Author(s), under exclusive licence to The Korean Society for Aeronautical & Space Sciences 2024.
PY - 2024/10
Y1 - 2024/10
N2 - The deformation of spinning projectiles induces alterations in their aerodynamic characteristics, thereby influencing flight stability. To assess the stability of spinning projectiles, the kernel extreme learning machine (KELM) is employed to develop the aerodynamic model of spinning projectiles. A mixed kernel is formulated by incorporating Gaussian and polynomial kernel functions to enhance the generalization ability of the model. The parameters of model are subsequently optimized using the cuckoo search (CS). Based on verifying the accuracy of the model by comparing the prediction results with the CFD results, the Lyapunov exponent method is adopted to investigate the impact of elastic deformation on the nonlinear angular motion stability of spinning projectiles, thereby revealing the mechanism of deformation on the attraction basin and stability for the angular motion. The findings reveal that the CS-based KELM with mixed kernel exhibits good reliability and accuracy in predicting the aerodynamic characteristics of spinning projectiles, with the maximum error between the predicted results and the CFD results remaining below 5%; as the deformation amplitude increases, the deformation-induced variation of yawing moment plays a leading role in the reduction of attraction basin; during the transition from convergence to divergence in the angular motion, the deformation can induce cluster oscillations prior to divergence, where the deformation-induced decrease of pitching damping moment significantly shapes the progression of the angular motion instability.
AB - The deformation of spinning projectiles induces alterations in their aerodynamic characteristics, thereby influencing flight stability. To assess the stability of spinning projectiles, the kernel extreme learning machine (KELM) is employed to develop the aerodynamic model of spinning projectiles. A mixed kernel is formulated by incorporating Gaussian and polynomial kernel functions to enhance the generalization ability of the model. The parameters of model are subsequently optimized using the cuckoo search (CS). Based on verifying the accuracy of the model by comparing the prediction results with the CFD results, the Lyapunov exponent method is adopted to investigate the impact of elastic deformation on the nonlinear angular motion stability of spinning projectiles, thereby revealing the mechanism of deformation on the attraction basin and stability for the angular motion. The findings reveal that the CS-based KELM with mixed kernel exhibits good reliability and accuracy in predicting the aerodynamic characteristics of spinning projectiles, with the maximum error between the predicted results and the CFD results remaining below 5%; as the deformation amplitude increases, the deformation-induced variation of yawing moment plays a leading role in the reduction of attraction basin; during the transition from convergence to divergence in the angular motion, the deformation can induce cluster oscillations prior to divergence, where the deformation-induced decrease of pitching damping moment significantly shapes the progression of the angular motion instability.
KW - Aerodynamic model
KW - Cuckoo search
KW - Dynamic stability
KW - Kernel extreme learning machine
KW - Nonlinear angular motion
KW - Spinning projectile
UR - http://www.scopus.com/inward/record.url?scp=85191409755&partnerID=8YFLogxK
U2 - 10.1007/s42405-024-00731-7
DO - 10.1007/s42405-024-00731-7
M3 - Article
AN - SCOPUS:85191409755
SN - 2093-274X
VL - 25
SP - 1219
EP - 1231
JO - International Journal of Aeronautical and Space Sciences
JF - International Journal of Aeronautical and Space Sciences
IS - 4
ER -