Adhoc geo-fiducial mats for landing UAVs

1. An apparatus for visual navigation of an unmanned aerial vehicle (UAV), the apparatus comprising:

a geo-fiducial mat including:

a landing pad region that provides a location for aligning with a landing pad of the UAV; and

a survey point indicated on the geo-fiducial mat; and

a plurality of geo-fiducials disposed in or about the landing pad region and each specified for a unique directional and offset position relative to the survey point, wherein the geo-fiducials each includes a two-dimensional (2D) pattern that visually conveys an alphanumerical code, wherein the 2D pattern has a shape from which an optical navigation system of the UAV can visually triangulate a position of the UAV.

2. The apparatus of claim 1 , wherein the geo-fiducials comprise at least three geo-fiducials that each convey a different alphanumerical code and are disposed at three different corners or along three different sides of the landing pad region.

3. The apparatus of claim 1 , wherein the geo-fiducials comprise:

first geo-fiducials having a first size that are configured to be disposed on or attached to the landing pad.

4. The apparatus of claim 3 , wherein the geo-fiducials further comprise:

second geo-fiducials having a second size, larger than the first size, the second geo-fiducials positioned further from a center of the landing pad region than the first geo-fiducials.

5. The apparatus of claim 4 , wherein the geo-fiducials further comprise:

third geo-fiducials having a third size, larger than the first and second sizes, the third geo-fiducials positioned further from the center of the landing pad region than the first and second geo-fiducials.

6. The apparatus of claim 4 , wherein the landing pad region comprises a rectangular shaped region, wherein the first geo-fiducials are disposed proximate to corners of the landing pad region, and wherein the second geo-fiducials are substantially centered along sides of the landing pad region.

7. The apparatus of claim 4 , wherein the second geo-fiducials are integrated into the geo-fiducial mat while the first geo-fiducials are configured to be physically distinct and separate from the geo-fiducial mat for adhering to or otherwise disposing on the landing pad of the UAV.

8. The apparatus of claim 1 , wherein the geo-fiducial mat further includes:

a directional marker disposed on the geo-fiducial mat for aligning the geo-fiducial mat with a predetermined direction such that positions of the geo-fiducials are determinable based upon location information of the survey point and the unique directional and offset position specified for each of the geo-fiducials.

9. The apparatus of claim 1 , wherein the geo-fiducial mat further includes:

alignment markings disposed on the geo-fiducial mat for indicating the landing pad region and aiding alignment of the landing pad to the landing pad region.

10. The apparatus of claim 1 , wherein the alphanumerical code conveyed by each of the geo-fiducials shares a common first portion that is associated with a pad identification of the landing pad and a different second portion that individually distinguishes each of the geo-fiducials of the geo-fiducial mat from each other.

11. The apparatus of claim 10 , wherein the pad identification includes:

a first segment having a value indicating that the geo-fiducials are not individually surveyed, but rather locations of the geo-fiducials are computable based at least in part upon location information of the survey point; and

a second segment that matches the common first portion of the alphanumerical code of each of the geo-fiducials.

12. The apparatus of claim 1 , wherein the geo-fiducial mat comprises a flexible substrate material that is amenable to rolling or folding.

13. The apparatus of claim 1 , wherein the geo-fiducial mat comprises puzzle sections that are separable.

14. A system for navigating an unmanned aerial vehicle (UAV) during landing or takeoff, the system comprising:

a charging pad for charging the UAV;

a geo-fiducial mat including:

a landing pad region that provides a location for aligning the charging pad with the geo-fiducial mat; and

a survey point indicated on the geo-fiducial mat; and

a plurality of geo-fiducials disposed in or about the charging pad region and each specified for a unique directional and offset position relative to the survey point, wherein the geo-fiducials each includes a two-dimensional (2D) pattern that visually conveys an alphanumerical code different from each other, wherein the 2D pattern has a shape from which an optical navigation system of the UAV can visually triangulate a position of the UAV.

15. The system of claim 14 , wherein the geo-fiducials comprise:

first geo-fiducials having a first size that are configured to be disposed on or attached to the charging pad.

16. The system of claim 14 , wherein the geo-fiducials comprise:

first geo-fiducials having a first size;

second geo-fiducials having a second size, larger than the first size, the second geo-fiducials positioned further from a center of the landing pad region than the first geo-fiducials; and

third geo-fiducials having a third size, larger than the first and second sizes, the third geo-fiducials positioned further from the center of the landing pad region than the first and second geo-fiducials.

17. The system of claim 16 , wherein the landing pad region comprises a rectangular shaped region, wherein the first geo-fiducials are disposed proximate to corners of the landing pad region, and wherein the second and third geo-fiducials are substantially centered along sides of the landing pad region.

18. The system of claim 16 , wherein the second and third geo-fiducials are integrated into the geo-fiducial mat while the first geo-fiducials are configured to be physically distinct and separate from the geo-fiducial mat for adhering to or otherwise disposing on the charging pad of the UAV.

19. The system of claim 14 , wherein the geo-fiducial mat further includes:

a directional marker disposed on the geo-fiducial mat for aligning the geo-fiducial mat with a predetermined direction such that positions of the geo-fiducials are determinable based upon location information of the survey point and the unique directional and offset position specified for each of the geo-fiducials; and

alignment markings disposed on the geo-fiducial mat for indicating the landing pad region and aiding alignment of the charging pad to the landing pad region.

20. The system of claim 14 , wherein the alphanumerical code conveyed by each of the geo-fiducials shares a common first portion that is associated with a pad identification of the landing pad and a different second portion that individually distinguishes each of the geo-fiducials of the geo-fiducial mat from each other.

21. The system of claim 20 , further comprising the UAV, wherein the UAV includes a controller coupled to memory storing instructions that when executed by the controller cause the UAV to perform operations comprising:

identifying a first segment of the pad identification as indicating that the charging pad has multiple geo-fiducials associated with the charging pad that are not individually surveyed;

computing locations for the geo-fiducials based at least in part upon location information of the survey point received by the UAV and the unique directional and offset position specified for each of the geo-fiducials; and

populating a geo-fiducial map stored within the UAV with the locations for the geo-fiducials.

22. The system of claim 14 , further comprising the UAV, wherein the UAV includes a controller coupled to memory storing instructions that when executed by the controller cause the UAV to perform operations comprising:

flying the UAV to a takeoff way point above the geo-fiducial mat;

visually triangulating the position of the UAV with the optical navigation system based upon one or more of the geo-fiducials; and

validating correct operation of a global positioning system (GPS) sensor at the takeoff waypoint based upon the position that is visually triangulated.