Mobile self-leveling landing platform for small-scale UAVS

• US 10,343,794 B2
• Filed: 06/18/2018
• Issued: 07/09/2019
• Est. Priority Date: 06/20/2014
• Status: Expired due to Fees

• Current Assignee: University of Denver
• Original Assignee: University of Denver
• Inventors: Conyers, Stephen A., Vitzilaios, Nikolaos, Rutherford, Matthew J., Valavanis, Kimon P.
• Primary Examiner(s): Knutson, Jacob D
• Application Number:
  US16/011,264
• Publication Number:
  US 20190009925A1
• Time in Patent Office: 386 Days
• Field of Search: 180233
• CPC Class Codes: B60K 1/02 comprising more than one electric motor
• CPC Class Codes: B62D 7/144 for vehicles with more than two axles
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64F 1/007 Helicopter portable landing pads
• CPC Class Codes: B64F 1/10 using self-propelled vehicles
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/17 Helicopters flying platforms B64U10/13
• CPC Class Codes: B64U 70/00 Launching, take-off or landing arrangements
• CPC Class Codes: B64U 70/90 Launching from or landing on platforms
• CPC Class Codes: B64U 80/86 Land vehicles
• CPC Class Codes: H02J 7/35 with light sensitive cells
• CPC Class Codes: H02S 99/00 Subject matter not provided for in other groups of this subclass
• CPC Class Codes: Y02E 10/50 Photovoltaic [PV] energy

Abstract

A mobile self-leveling landing platform vehicle is disclosed that includes a landing surface and one or more wheel assemblies. Each wheel assembly includes a wheel, a control arm coupled with the wheel and the body of the landing platform vehicle, and an actuator coupled with the control arm and the body of the platform vehicle. Methods for self-leveling the landing platform vehicle are also disclosed.

Claims

1. A mobile landing platform vehicle comprising:

a landing platform body;

a landing platform surface of the landing platform body;

an inclinometer;

a first actuating wheel assembly including a first wheel, a first control arm coupled with the first wheel, and a first linear actuator coupled with the landing platform body and the first control arm;

a second actuating wheel assembly including a second wheel, a second control arm coupled with the second wheel, and a second linear actuator coupled with the landing platform body and the second control arm;

a third actuating wheel assembly including a third wheel, a third control arm coupled with the third wheel, and a third linear actuator coupled with the landing platform body and the third control arm;

a fourth actuating wheel assembly including a fourth wheel, a fourth control arm coupled with the fourth wheel, and a fourth linear actuator coupled with the landing platform body and the fourth control arm; and

a controller communicatively coupled with the inclinometer, the first actuator, the second actuator, the third actuator, and the fourth actuator, the controller configured to determine and send at least one adjustment value to the first actuator, the second actuator, the third actuator, and the fourth actuator to maintain the landing platform surface level.

2. The mobile landing platform vehicle as claimed in claim 1, wherein the at least one adjustment value is determined from data received from the inclinometer.

3. The mobile landing platform vehicle as claimed in claim 1, wherein the inclinometer comprises a dual axis inclinometer.

4. A mobile landing platform vehicle comprising:

a landing platform body having a landing platform surface;

four actuating wheel assemblies coupled with the landing platform body, each actuating wheel assembly comprising;

a wheel;

a control arm coupled with the wheel and the landing platform body; and

an actuator coupled with the control arm and the landing platform body;

an inclinometer; and

a controller coupled with the inclinometer and each actuator of the four actuating wheel assemblies, wherein the controller is configured to keep the landing platform surface level based on inclination data received from the inclinometer and by sending control signals to the actuators of the four actuating wheel assemblies.

5. The mobile landing platform vehicle as claimed in claim 4, wherein each actuating wheel assembly further comprises a wheel motor coupled with the respective control arm and the respective wheel, each wheel motor configured to rotate the respective wheel of each actuating wheel assembly.

6. The mobile landing platform vehicle as claimed in claim 4, wherein the inclinometer comprises a dual axis inclinometer.

7. The mobile landing platform vehicle as claimed in claim 4, wherein each of the four actuating wheel assemblies comprise a linear actuator controller in communication with the controller.

8. The mobile landing platform vehicle as claimed in claim 4, wherein each of the four actuating wheel assemblies may send position feedback signals that indicate the position of the respective actuating wheel assembly.

9. The mobile landing platform vehicle as claimed in claim 4, further comprising:

one or more batteries; and

one or more solar cells disposed on the landing platform surface electrically coupled with the one or more batteries.

10. The mobile landing platform vehicle as claimed in claim 9, wherein the controller is configured to tilt the landing platform surface at an angle relative to horizontal that produces an increased power from the one or more solar cells.

11. The mobile landing platform vehicle as claimed in claim 4, wherein the landing platform further comprises a plurality of flaps that extend from the landing platform surface to increase the surface area of the landing platform surface.