A linear programming-based dynamic inverse attitude and velocity control method was developed for tiltrotor aircraft operating in helicopter mode with a small degree of nacelle tilting.

• 为了研究倾转旋翼飞机短舱倾转过程中的飞行控制问题,提出了一种基于线性规划的动态逆方法,以实现直升机模态下短舱小角度倾转时的姿态和速度控制。