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Advanced flight control system and method for jet aircraft power mode 3

机译:喷气飞机动力模式的先进飞行控制系统和方法3

摘要

How to stabilize the jet power mode 3 aircraft when you sail in fixed wing mode helicopter mode, jet power mode 3 aircraft and composite mode, is disclosed. Velocity vector component values ​​of multiple derived from the sequences that have been instruction (2) the way passing the target point or controller, to the operation of the pilot of either (1) a number and contains the velocity vector command, this method is fully automated these is used in flight is, and a rotor speed reference value further decreased with increasing forward speed to reduce the load on the rotor, which allows the conditions for stopping the rotor in flight thereby. Control of the swash plate of the rotor, stability of the velocity vector, which is the instruction is implemented in the flight mode and all using a combination of mixed aerodynamic controls such as horizontal tail Erubon, canards, and the rudder. Stable to velocity vectors are instructions include multiple control constraints applied to the stick controller of the pilots to prevent penetration of the limit range.
机译:公开了当以固定翼模式直升机模式,喷气动力模式3飞机和复合模式航行时如何稳定喷气动力模式3飞机。速度矢量分量值的倍数是从已通过指令(2)通过目标点或控制器的方式到(1)个数字的飞行员操作的序列中得出的,并且包含速度矢量命令的,此方法在完全自动化的情况下,这些是在飞行中使用的,并且转子速度参考值随着前进速度的增加而进一步减小,以减小转子上的负载,从而允许在飞行中停止转子的条件。在飞行模式下实现对转子斜盘的控制,速度矢量的稳定性(该指令是在飞行模式下实现的),并且全部使用混合气动控制(如水平尾翼Erubon,鸭翼和方向舵)进行组合。对速度矢量稳定的指令包括应用于飞行员的操纵杆控制器的多个控制约束,以防止超出极限范围。

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