06.1 - Flight Dynamics and Control (Control & Modelling)
REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS
C.-K. Zhou¹, Z.-F. Luo¹, T. Zhang¹; ¹SUN YAT-SEN UNIVERSITY, China
Flexible skin is a future trend in morphing aircraft. This study explores its application to hypersonic lifting bodies. Deformable shapes are modeled using parameterized equations(CST). Aerodynamic parameters are obtained through CFD. Relative optimal reentry trajectories are optimized using Gaussian Pseudo method. Results show advantages in specific mission scenarios.