Auto Credit Based on Jundroo's P-51-D
This project took me a lot of time, and I adjusted it for a long time. All command data is in variables. You can copy all functions to your aircraft and use this inertial navigation system.
NOTE: if this inertial navigation system is moved to a snow mountain, it will make an error. I will enter the changed variables into the comment.
Specifications
Spotlights
- CR929thenewSPplayer 1.6 years ago
- TermineanIndustries 2 months ago
General Characteristics
- Predecessor P-51-D
- Created On Android
- Wingspan 38.9ft (11.9m)
- Length 33.9ft (10.3m)
- Height 12.4ft (3.8m)
- Empty Weight 8,883lbs (4,029kg)
- Loaded Weight 9,075lbs (4,116kg)
Performance
- Horse Power/Weight Ratio 0.225
- Wing Loading 36.5lbs/ft2 (178.2kg/m2)
- Wing Area 248.6ft2 (23.1m2)
- Drag Points 3681
Parts
- Number of Parts 188
- Control Surfaces 14
- Performance Cost 886
You can adjust the calibration speed of the inertial navigation system. The variable is "spd". The default is 100 (that is, calibrate 100 meters per second), which can be adjusted by yourself.
LOT|abs((LOA*clamp01(abs(floor(LOA))>0))/(rate(LOA)+clamp01(abs(floor(LOA))=0))clamp01(abs(floor(LOA))>0))
LAT|abs((LAA*clamp01(abs(floor(LAA))>0))/(rate(LAA)+clamp01(abs(floor(LAA))=0))*clamp01(abs(floor(LAA))>0))