to lazy to add description so here's the code:
clamp(smooth(Pitch,.5) + ((PitchAngle/45)-((sin(Heading+0)*rate(Longitude))+(cos(Heading+0)*rate(Latitude)))/40)-PitchRate/80,-1,1)
and
clamp(smooth(Roll,.5) + ((RollAngle/45)-((sin(Heading+90)*rate(Longitude))+(cos(Heading+90)*rate(Latitude)))/40)+RollRate/80,-1,1)
(a simpler version of this code was also used in my other post 'sir Andrew')
Specifications
General Characteristics
- Successors 1 airplane(s) +14 bonus
- Created On Android
- Wingspan 5.2ft (1.6m)
- Length 24.8ft (7.6m)
- Height 7.3ft (2.2m)
- Empty Weight 466lbs (211kg)
- Loaded Weight 9,103lbs (4,129kg)
Performance
- Power/Weight Ratio 5.165
- Wing Loading 1,258.8lbs/ft2 (6,145.9kg/m2)
- Wing Area 7.2ft2 (0.7m2)
- Drag Points 1071
Parts
- Number of Parts 25
- Control Surfaces 1
- Performance Cost 177
@FairFireFight I dont think this is worth your time but I want to show your concept without using a gyro or a rotator
thanks! @tylerdeveneuxmusic