Multiconstrained Ascent Trajectory Optimization Using an Improved Particle Swarm Optimization Method

This paper researches the ascent trajectory optimization problem in view of multiple constraints that effect on the launch vehicle. First, a series of common constraints that effect on the ascent trajectory are formulated for the trajectory optimization problem. Then, in order to reduce the computat...

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Bibliographic Details
Main Authors: Mu Lin, Zhao-Huanyu Zhang, Hongyu Zhou, Yongtao Shui
Format: Article
Language:English
Published: Hindawi Limited 2021-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2021/6647440