# 结果监视6个量
- TwrTpTDxi
	- 塔架顶点/偏航轴前后（平移）偏转量（相对于未偏转位置），包括所有平台运动
- TwrTpTDzi
	- Tower-top / yaw bearing axial (translational) deflection (relative to the undeflected position) including all platform motions
- YawBrTVxp
	- Tower-top / yaw bearing fore-aft (translational) **velocity** (absolute)
- YawBrTVzp
	- Tower-top / yaw bearing axial (translational) **velocity** (absolute)
- PtfmRDyi
	- Platform pitch tilt angular (rotational) displacement. In ADAMS, it is output as an Euler angle computed as the 2nd rotation in the yaw-pitch-roll rotation sequence. It is not output as an Euler angle in FAST, which assumes small rotational platform displacements, so that the rotation sequence does not matter.
	- 平台俯仰倾斜角位移（旋转）。在 ADAMS 中，它作为欧拉角输出，计算为 yaw-pitch-roll 旋转序列中的第二个旋转。在 FAST 中，它不以欧拉角输出，因为 FAST 假设平台的旋转位移很小，因此旋转顺序无关紧要。
- PtfmRVyt
	- Platform pitch tilt angular (rotational) velocity


##  TwrTpTDzi
```
m%AllOuts(TwrTpTDxi) =     m%RtHS%rO(1) - y%TowerLn2Mesh%Position(1,J)
m%AllOuts(TwrTpTDzi) =     m%RtHS%rO(2) - y%TowerLn2Mesh%Position(3,J) + p%PtfmRefzt
```

rO      !< Position vector from inertial frame origin to tower-top / base plate (point O) [m]

## YawBrTVxp YawBrTVzp 前后 Yaw平动速度
```
m%AllOuts(YawBrTVxp) =  DOT_PRODUCT( m%RtHS%LinVelEO, m%CoordSys%b1 )
m%AllOuts(YawBrTVzp) =  DOT_PRODUCT( m%RtHS%LinVelEO, m%CoordSys%b2 )
```

LinVelEO      !< Linear velocity of the base plate (point O) in the inertia frame (body E for earth) [-]
b1      !< Vector / direction b1 (=  xp from the IEC coord. system) [-]
b2      !< Vector / direction b2 (=  zp from the IEC coord. system) [-]

### LinVelEO 差距较大
```
rt_hs.lin_vel_eo = lin_vel_x_o.clone() + rt_hs.lin_vel_ez.clone();
for i in 0..NPX{
	rt_hs.lin_vel_eo = rt_hs.lin_vel_eo.clone() + x.qdt[PX[i] as usize - 1] * rt_hs.plin_vel_eo.slice(s![PX[i] - 1, 0, ..]).to_owned();
}
```

#### lin_vel_x_o有差距



#### rt_hs.lin_vel_ez有差距

### b1[3]少许差距

# pitch 角度 角速度
```
m%AllOuts( PtfmRDyi) = x%QT  (DOF_P )*R2D
m%AllOuts( PtfmRVyt) = -DOT_PRODUCT( m%RtHS%AngVelEX, m%CoordSys%a3 )*R2D
```

AngVelEX      !< Angular velocity of the platform (body X) in the inertia frame (body E for earth) [-]
a3      !< Vector / direction a3 (= -yt from the IEC coord. system) [-]