大连理工大学主页平台管理系统石岩 Transient-State Adaptive Optimal Control of Aircraft Engine Systems with Input Saturation 中文主页

石岩

访问量：

开通时间：..

最后更新时间：..

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果

Transient-State Adaptive Optimal Control of Aircraft Engine Systems with Input Saturation

点击次数：

发布时间：2024-11-04

发表时间：2024-11-01

发表刊物：IEEE Transactions on Aerospace and Electronic Systems

ISSN号：0018-9251

上一条：Improved real-time H∞ control for aero-engines based on the equilibrium manifold expansion model

下一条：Starting Control of Free Piston Engine Linear Generator Based on Simulated annealing Algorithm to Optimize Fractional PID