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  5. Optimum control of flight simulator along pitch and yaw axes taking into account structural resource

Optimum control of flight simulator along pitch and yaw axes taking into account structural resource

V.V. Kabanyachyi
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Problem statement and finding technique of optimum dependences of pitch and yaw axes co-ordinates of six degree of freedom motion system of flight simulator within flight simulators is bring. Due to use of priority circuit of motion cueing along degrees of freedom the optimum dependences of pitch and yaw axes co-ordinates enable more effective use of structural resource of six degree of freedom motion system for physical modelling of aircraft dynamic properties on flight simulators and approach the motion cues to the real.
Keywords: six degree of freedom motion system, flight simulator, physical modelling of aircraft dynamic properties