System and method for adjustable ballast

1. A method of adjusting a center of gravity (CG) of an aircraft, the method comprising:

inputting at least one load parameter into a flight computer;

determining, via a processer of the flight computer, the CG of the aircraft;

responsive to a determination by the processor that the CG is outside of a CG envelope, moving at least a first movable ballast of a plurality of movable ballasts from a first ballast dock to a second ballast dock to move the CG toward the CG envelope; and

wherein each of the first and second ballast docks comprise a housing and a first ballast tray secured within the housing, the first ballast tray comprising a plurality of channels.

2. The method of claim 1 , wherein the at least one load parameter comprises one or more of a fuel parameter, a passenger parameter, a cargo parameter, and a ballast parameter.

3. The method of claim 1 , wherein the at least one load parameter includes a weight and a location of the weight.

4. The method of claim 1 , comprising:

determining, via a processer of the flight computer, the CG of the aircraft after the moving the at least the first movable ballast; and

responsive to a determination by the processor that the CG is still outside of a CG envelope, moving at least a second movable ballast of the plurality of movable ballasts from the first ballast dock to the second ballast dock to move the CG toward the CG envelope.

5. The method of claim 1 , comprising responsive to a determination by the processor that the CG is inside of the CG envelope, moving at least the first movable ballast of the plurality of movable ballasts from the first ballast dock to the second ballast dock to move the CG away from a periphery of the CG envelope.

6. The method of claim 1 , wherein the moving the first movable ballast comprises securing the first movable ballast in the second ballast dock with a pin that passes through bores of the housing and the first movable ballast.

7. The method of claim 1 , wherein each channel of the plurality of channels comprises a different width and depth so that only one movable ballast of the plurality of movable ballasts can fit within a particular channel of the plurality of channels.

8. The method of claim 1 , wherein each housing of the first and second ballast docks comprises a cut out configured to expose a portion of the plurality of movable ballasts when the plurality of movable ballasts are inserted into either of the first and second ballast docks.

9. The method of claim 1 , wherein the plurality of movable ballasts comprises a first, second, and third ballast.

10. The method of claim 9 , wherein the first and second ballasts have a first weight and the third ballast has a second weight.

11. The method of claim 9 , wherein each movable ballast of the plurality of movable ballasts has a different weight.

12. The method of claim 1 , wherein the first ballast dock is secured to the aircraft fore of the CG of the aircraft and the second ballast dock is secured to the aircraft aft of the CG of the aircraft.

13. The method of claim 1 , wherein the first ballast dock is secured to the aircraft fore of the second ballast dock and the second ballast dock is secured aft of the CG of the aircraft.

14. The method of claim 13 , wherein the first ballast dock is secured to the aircraft aft of the CG of the aircraft.

15. The method of claim 1 , comprising

wherein each of the first and second ballast docks comprise a second ballast tray secured within the housing and comprising a plurality of channels; and

wherein opposing channels of the first and second ballast trays form bays configured to receive a movable ballast of the plurality of movable ballasts.

16. The method of claim 1 , wherein the first ballast tray is made of a material selected from the group consisting of rubbers, plastics, and polymers.

17. The method of claim 1 , wherein the first ballast tray is coated with a material selected from the group consisting of rubbers, plastics, and polymers.