Analytic target cascading with fuzzy uncertainties based on global sensitivity analysis for overall design of launch vehicle powered by hybrid rocket motor
Authors:
- Pengcheng WangPWPengcheng Wang
- Hao ZhuHZHao Zhu
- Hui TianHTHui Tian
- Guobiao CaiGCGuobiao Cai
- 1 July 2021
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 114
Abstract
No abstract availableKeywords
Funding Information
- Aeronautical Science Foundation of China (20180151001)
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