System to accelerate and decelerate aircraft for take-off and landing

1. A system for controlling movement of an aircraft, the system comprising:

a platform for supporting the aircraft;

a clamp mechanism coupled to the platform to releasably couple the aircraft onto the platform, the clamp mechanism including at least one wheel block, the wheel block positioned on opposing sides of at least a front wheel of the aircraft and configured to prevent the front wheel from rolling;

a conveying system coupled to the platform and configured to:

with the aircraft coupled to the platform during take-off of the aircraft, move the platform to accelerate the aircraft or to decelerate the aircraft; and

during landing of the aircraft, decelerate the aircraft; and

a controller coupled to the clamp mechanism and to the conveying system, the controller configured to communicate with the clamp mechanism and with the conveying system to control:

acceleration of the platform during take-off of the aircraft; and

deceleration of the platform during landing of the aircraft.

2. The system of claim 1 , wherein the platform is positioned within a recess and above a floor of the recess, and wherein the recess is defined in a surface of a taxiway.

3. The system of claim 2 , wherein the conveying system comprises:

at least one rail positioned in a direction along a length of the floor of the recess; and

an electrical power supply electrically connected to the at least one rail.

4. The system of claim 1 , further comprising a frame positioned above a runway and extending across a width of the runway, the frame coupled to the platform and to the conveying system, wherein the conveying system further comprises:

wheels coupled to rotate relative to the platform;

a first rail positioned on a first side of the runway;

a second rail positioned on a second side of the runway; and

an electrical power supply electrically connected to the first rail and the second rail.

5. The system of claim 1 , wherein the platform comprises a first component spaced apart from a second component, and wherein the conveying system comprises a first propulsion driving mechanism coupled to the first component and a second propulsion driving mechanism coupled to the second component.

6. The system of claim 1 , wherein the platform comprises a first component spaced apart from a second component, and wherein the clamp mechanism comprises at least one clamp mechanism coupled to the first component and another clamp mechanism coupled to the second component, the other clamp mechanism distinct from the at least one clamp mechanism.

7. The system of claim 1 , wherein the platform comprises a first component, a second component, and a third component, the second component spaced apart from the first component and from the third component and the first component spaced apart from the third component, wherein the clamp mechanism comprises:

a first clamp mechanism coupled to the first component,

a second clamp mechanism coupled to the second component, and

a third clamp mechanism coupled to the third component, and

wherein the controller is in communication with the first clamp mechanism, the second clamp mechanism, the third clamp mechanism, and the conveying system.

8. The system of claim 1 , wherein the platform comprises a first component, a second component, and a third component, the second component spaced apart from the first component and from the third component and the first component spaced apart from the third component, and wherein the conveying system comprises a first propulsion driving mechanism coupled to the first component, a second propulsion mechanism coupled to the second component, and a third propulsion mechanism coupled to the third component.

9. The system of claim 1 , wherein the conveying system comprises a propulsion driving mechanism coupled to the platform.

10. The system of claim 1 , wherein the platform comprises at least a portion of a top surface positioned in angular relationship relative to a surface on which the platform is positioned.

11. The system of claim 1 , wherein the clamp mechanism is coupled to at least one landing gear of the aircraft during acceleration or deceleration of the platform and decoupled from the landing gear to permit aircraft to lift off of the platform at take-off or for the aircraft to taxi off of the platform.

12. The system of claim 1 , further comprising a plurality of sensors positioned about the platform and in communication with the controller, the plurality of sensors configured to sense positions of wheels on front landing gear of the aircraft and to sense positions of wheels on rear landing gear of the aircraft, wherein to receive the aircraft onto the platform during the landing of the aircraft, the controller is further configured to adjust the platform to match speed, position, and orientation of the aircraft.

13. The system of claim 1 , wherein the controller is further configured to, during the landing of the aircraft and in response to data received from a plurality of sensors positioned about the platform, control movement of a top surface of the platform to match an orientation of the aircraft in order to receive the aircraft onto the platform.

14. The system of claim 13 , wherein a top surface of the platform is oriented to match a pitch, a yaw, a roll, or a combination thereof, of the aircraft to receive the aircraft onto the platform.