System approach to the certification of dynamic stands of complex aircraft simulators
Journal Title: Механіка гіроскопічних систем - Year 2018, Vol 0, Issue 35
Abstract
On the basis of motion cueing problem, which is reduced to synthesis of program signal that minimizes function evaluating a coincidence error of perception of motion cues on aircraft and flight simulator, and takes into account that movement of motion system is within operating movement range of motion system, motion system characteristic is within permissible determination region of motion system characteristics, that is, region within which motion normalized quality of motion system is ensured, and motion cue sign on flight simulator coincides with motion cue perceived on aircraft, based on system approach the problem of certification of motion system of aircraft flight simulators was formulated, taking into account: - method of motion cueing along separate degrees of freedom that provides motion cueing as close as it is possible to real one in terms of characteristic signs (character and direction of motion perception, time of motion perception beginning on aircraft and flight simulator, intensity and duration of motion cues); - maximum use of energy and structural resources of motion system; - determination of motion system characteristics complex, which evaluate its suitability to motion cueing, and their normalization, that is, determination of permissible determination region of motion system characteristics. This approach takes into account the motion cueing method according to separate degrees of freedom, optimum use of both structural and energy resources of motion systems, and a set of motion system characteristics. The developed approach was used during design, testing and certification of flight simulators of aircraft Ilushin-96-300 and Typolev-204 (Russia, Penza’ modeling design bureau), Antonov‑74TK-200 and Antonov-140 (Ukraine, state enterprise «Antonov»).
Authors and Affiliations
V. V. Kabanyachiy
Keywords
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