optimum adaptive control

基本解釋

This paper presents a new design for airplane cabin pressure, i. e. the optimum and adaptive control for airplane cabin pressure.
本文提出了飛機座艙壓力控制的新設(shè)計方案，即飛機座艙壓力的最佳控制與自適應(yīng)控制。
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Recently, several control modes like optimum control, adaptive control , differential geometry control and etc are available for the STATCOM control , but each has its shortcoming.
STATCOM目前控制方式有最優(yōu)控制、自適應(yīng)控制、微分幾何控制等方式，但各種控制方式都有其缺點。
Finally, after rigorous theoretical analysis on load automatically adaptive principle, thesis approaches the optimum tracing control principle.
最后，對負載自動適應(yīng)機理進行了深入的理論分析，給出了合理的最優(yōu)跟蹤控制策略。