A Multivariable Control Method for Aeroengine with H∞ Performance Based on Fully Adjustable Lstm-RbfnnShancheng Li,Yong Wang,Haibo ZHANGcrossref（2024）引用 0|浏览24AI 理解论文溯源树样例生成溯源树，研究论文发展脉络Chat Paper正在生成论文摘要
