研究直升机悬停状态时其动力学模型非最小相位且不稳定特性的设计问题。

A study on the method of design is presented for helicopter hover with nonminimumphase unstable characteristics.

youdao

研究直升机悬停状态时其动力学模型非最小相位且不稳定特性的设计问题。

A study on the method of design is presented for helicopter hover with nonminimumphase unstable characteristics.

youdao