A flight simulator for ground training of Cessna Citation 500 aircraft is addressed. In order to acquire the necessary information in the relatively short period of time available for the execution of the flight tests and the analysis, use was made intensively of dynamic flight test techniques in relation with computer data processing. The mathematical models to be identified must give an adequate description of the aerodynamic forces and moments, the engine characteristics, the flight control system and the landing gear characteristics. In order to evaluate and test the general models, both offline and online (pilot in the loop) simulations were performed on the computer and moving base flight simulator. Comparisons were made between the measured flight test time histories and the computed model responses. The employed instrumentation system, the flight test program, the data processing and corresponding parameter identification and the synthesis of the various models, are presented.
Phase 2 Flight Simulator Mathematical Model and Data-Package, Based on Flight Test and Simulation Techniques
1989
18 pages
Report
Keine Angabe
Englisch