A Modified Robust Homotopic Method for the Low-Thrust Fuel-Optimal Orbital Control Problem

A Modified Robust Homotopic Method for the Low-Thrust Fuel-Optimal Orbital Control Problem

This study focuses on improving the application of the quadratic penalty smoothing technique for solving the fuel-optimal problem of low-thrust trajectory. Some practical techniques, including the Particle Swarm Optimization algorithm (PSO), the co-state normalization technique, and the single shoot...

Full description

Bibliographic Details
Main Authors: Yuyang Huang, Lifei Zhang, Xianjian Zhang
Format: Article
Language:English
Published: MDPI AG 2024-09-01
Series:Aerospace
Subjects:
low-thrust trajectory optimization
homotopic method
fuel-optimal problem
energy-optimal problem
homotopic iteration strategy
optimal control
Online Access:https://www.mdpi.com/2226-4310/11/9/766

Internet

https://www.mdpi.com/2226-4310/11/9/766

Similar Items