According to the work principle, the theory model of the shell bodys rollattitude detection is built.
依据加速度计的工作原理,建立了弹体滚装姿态探测理论模型。
2
INNER LOOP control, For autopilot operation this is the basis control of airplane pitch and rollattitude without regard to flight path.
内环路控制,对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿态和坡度的基本控制。
3
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the rollattitude protection system works as expected.