Method and device for determining the dynamic stability margin of an aircraft
SD MP CG O SD MP O ααMPA method of determining a dynamic stability margin Mof an aircraft includes calculating the longitudinal position Xof a maneuver point MP to find the distance between the maneuver point and the position Xof the aircraft center of gravity CG, as a function of the angular veloci...
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| Format: | Patent |
| Sprache: | eng |
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