Find, for a given static flight condition (climb, cruise or descent), the required trim angle versus weight and center of gravity positions. The code works for FSX aircraft and it is for MATLAB.
Users are required to extract data from aircraft.cfg and .air file (using AAM). See the wiki pages for more details.
Copy the clone FSXstability to any directory. Rember to add the new direxctory to MATLAB's path.
From inside MATLAB run one of the following script:
- testISA.m : generates ISA 1962 profiles for pressure, density, temperature and speed of sound up to 31 km. UK unit.
- stability_snapshot.m : find elevator trim angle for a given weight and flight condition.
- CG_trim.m : find the elevator trim angle envelope for different weight and center of gravity positions.
Licensed under the GPL v3.0 license.