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