The adaptive optimal decoupling control method of helicopter rotor concordant loading system was discussed.
研究了直升机旋翼协调加载系统的自适应最优解耦控制问题。
As a new approach an optimal decoupling control concept is presented which has the advantages of easy realization, few computational work and well real-time ability.
本文提出一种最佳解耦控制方法。它具有实现容易、计算量小、实时性好等优点。
As a new approach an optimal decoupling control concept is presented which has the advantages of easy realization, few computational work and well real-time ability.
本文提出一种最佳解耦控制方法。它具有实现容易、计算量小、实时性好等优点。
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