The attitude control optimization of small rocket

Abstract In this article, an optimization method for attitude calculation and vector control of small rocket is proposed, which reduces the performance requirements and costs of gyroscopes. Dynamic model parameters such as engine thrust curve and rocket body moment of inertia are added to the tradit...

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Bibliographic Details
Published inJournal of physics. Conference series Vol. 2235; no. 1; pp. 12013 - 12018
Main Authors Ni, Runfeng, Wen, Chunyu, Jia, Linhai, Zhang, Yao, Liu, Shiyu
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.05.2022
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