| 1. | The model developed here is suitable for the tilt rotor aircraft during hover , transition and cruise . the longitudinal equations of motion provide a foundation for further investigation on tilt - rotor flight dynamics 文中所建模型具有较高精度,适合于飞行包线内的所有模式,为倾转旋翼飞机飞行动力学的进一步研究提供了基础。 |