Impact Analysis of Different Trajectory Shapes on Optimization Based on Original Natural Algorithm

In this paper, the reentry phase of the Aerospaceplane is taken as the research object, and the performance parameters of the reusable rocket of a private company are analyzed. Aiming at the guidance and control scheme of the spacecraft returning to the reentry trajectory in the real environment, th...

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Bibliographic Details
Main Authors: Yijing Chen, Ying Nan, Zhihan Li
Format: Article
Language:English
Published: Wiley 2024-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2024/5569229
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