Synthetic Data Package development for FNPT-type simulator

Dynamic simulation models are proving increasingly realistic and reliable, to the extent that they can accurately and faithfully simulate the dynamic behavior of their real-world counterparts, even when the latter are still in the design phase. With this purpose, they are often employed to support the design phase by testing solutions that exist only on paper, resulting in obvious time and resource savings. This thesis carried out in collaboration with TXT E-Tech, aims to investigate the use of a fixed-wing aircraft flight dynamics simulation model to create a "Data Package" for the validation and certification of a "Flight Navigation Procedures Trainer" (FNPT) simulator in accordance with EASA regulations. According to the CS-FSTD(A) (Certification Specifications for Flight Simulator Training Device (Aircraft)), FNPT-type simulators are permitted to rely on data sources that are not directly tied to flight tests conducted on the specific aircraft or aircraft class being simulated. Consequently, this opens up new avenues for research into more accessible and economically feasible data sources. The aircraft classes under consideration comprises the A320-200 and Boeing 737-800 series, examined through official documents and static analyses using PACELAB APD software. The goal is to extract relevant data for conducting simulator certification tests. Specifically, the study focused on Climb AEO/OEI (All Engine Operative/One Engine Inoperative) performances, Engine acceleration/deceleration, Column/Wheel/Pedal position vs forces, Trim Calibration and Alignment of cockpit throttle lever vs selected engine parameter.