FRAMECALB159
The FrameCalb159 module is designed to compute the calibration constants used to determine the physical values of strain from the strain gauges located on the flange of the main wing rib and in the fuselage wing spar of the L159 aircraft. The computation is realized on grounds of the evaluation of the flight data recorded by the AMOS monitoring system's recorder.
FRAMECALB159 program module enables these basic functions:
- to select AMOS (D type) and FRAME (F type) files
- to set the (synchronization and test) computation constants
- to compute the time of depletion of outside tanks
- to compute instant weight of the aircraft from the initial amount of fuel in the fuselage fuel tank and the fuel flow
- to synchronize the data read from the AMOS (type D) and the FRAME (type F) files
- to filter the data according to the position of the flaps, engine pods, and Mach number
- to optionally filter the data according to the height
- to compute the load (from the synchronized data that went through filtration)
- to compute calibration constants, fitting errors, and other statistical data
- to evaluate the correctness of the calibration considering the number of fitted points and the fitting error