US Patent 7579966 Dual-axis loadmeter

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.