| 摘要 |
The present invention is directed to a computerized system that includes a graphical user interface (GUI) having a display and a data input device. The computerized system performs a method including the step of providing a plurality of aircraft parameters. At least one vertical g-force value is calculated in real time based on the plurality of aircraft parameters. A lateral g-force value is calculated in real time based on the plurality of aircraft parameters. The at least one vertical g-force value is displayed relative to at least one predetermined vertical reference value. The lateral g- force value is displayed relative to at least one predetermined lateral reference value.
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