Paper
6 November 2023 Optimization of the overall parameter integration design of electromagnetic launch vehicle trajectory
Xuemei Zhang
Author Affiliations +
Proceedings Volume 12921, Third International Computing Imaging Conference (CITA 2023); 129215C (2023) https://doi.org/10.1117/12.2692081
Event: Third International Computing Imaging Conference (CITA 2023), 2023, Sydney, Australia
Abstract
In order to make full use of the energy provided by the electromagnetic device during the launch of the launch vehicle, an integrated optimization design of the overall parameters/flight trajectory of the electromagnetic launch vehicle is proposed, a corresponding mathematical model is established, the integrated optimization design objective function and the optimized design variables are determined, and a two-loop iterative optimization algorithm based on the outer-loop Levenberg-Marquardt algorithm and the inner-loop Newton iteration method is applied to achieve the integrated optimization design of the overall parameters/flight trajectory of the electromagnetic launch vehicle. The simulation results show that the initial kinetic energy requirement provided by the electromagnetic orbit is reduced by 17.5%, which fully demonstrates the effectiveness of the algorithm.
© (2023) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Xuemei Zhang "Optimization of the overall parameter integration design of electromagnetic launch vehicle trajectory", Proc. SPIE 12921, Third International Computing Imaging Conference (CITA 2023), 129215C (6 November 2023); https://doi.org/10.1117/12.2692081
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Electromagnetism

Design and modelling

Mathematical optimization

Rockets

Mathematical modeling

Integration

Vacuum

Back to Top