GEO-FENCING
A balloon includes a cut-down device, a payload, and an envelope. A control system could be configured to determine a position of the balloon with respect to a predetermined zone. The cut-down device could be operable to cause at least the payload to land in response to determining that the position of the balloon is within the predetermined zone. The predetermined zone includes an exclusion zone and a shadow zone. The shadow zone could include locations from which the balloon would be likely to drift into the exclusion zone based on, e.g., historic weather patterns or expected environmental conditions. Boundaries of the shadow zone could be determined based on, for example, a probability of the balloon entering the exclusion zone.
1 . A method of preventing a payload of a balloon from entering an exclusion zone including a static volume of airspace over a first geographic area, and the method comprising:
identifying a set of locations from which a probability of the balloon entering the static volume of airspace is greater than a predetermined threshold value based on one or more environmental conditions, a speed of the balloon, and a heading of the balloon, wherein each location of the set of locations is outside of the static volume of airspace;
determining a shadow zone including the set of locations;
determining whether the balloon has entered the shadow zone; and
in response to determining that the balloon has entered the shadow zone causing, using a cut-down device, at least the payload to land outside of the first geographic area and thereby preventing the payload from entering the exclusion zone.
2 . The method of claim 1 , wherein the environmental conditions includes historical wind speed and direction.
3 . The method of claim 2 , wherein determining the shadow zone include determining static boundaries for the shadow zone based on the historical wind speed and direction.
4 . The method of claim 1 , wherein the environmental conditions includes current wind speed and direction.
5 . The method of claim 4 , wherein determining the shadow zone further includes adjusting one or more boundaries for the shadow zone based on the current wind speed and direction.
6 . The method of claim 1 , wherein the environmental conditions includes forecasted wind speed and direction.
7 . The method of claim 1 , wherein using the cut-down device includes severing the payload from a balloon envelope of the balloon.
8 . The method of claim 1 , wherein at least one boundary of the shadow zone remains static.
9 . The method of claim 8 , wherein the at least one boundary is a maximum operating altitude of the balloon.
10 . The method of claim 8 , wherein the at least one boundary is a minimum operating altitude of the balloon.
11 . The method of claim 1 , wherein the predetermined threshold value is a 50% likelihood that the balloon will enter the exclusion zone from a given location.
12 . The method of claim 1 , wherein after using the cut-down device, the balloon is blown in to the exclusion zone.
13 . The method of claim 1 , wherein identifying the set of locations includes using a plurality of Monte Carlo simulations.
14 . The method of claim 1 , wherein identifying the set of locations include generating a heat map representing likelihoods of the balloon entering the exclusion zone from points in three-dimensional space, and wherein the heat map is used to determine the shadow zone.
15 . The method of claim 1 , wherein using the cut-down device causes the balloon to land with the payload.
16 . The method of claim 1 , wherein determining the shadow zone includes determining boundaries of the shadow zone such that the boundaries of the shadow zone differ based on altitude.
17 . The method of claim 1 , wherein the boundaries of the shadow zone include at least one sloped zone to account for varying altitudinal wind data of the wind conditions.
18 . The method of claim 1 , wherein the boundaries of the shadow zone include at least one sloped zone to account for varying altitudinal wind data of the wind conditions.
19 . The method of claim 1 , wherein the boundaries of the shadow zone include at least one sloped zone to account for one of an ascent, descent, or lateral movement rate of the balloon.
20 . The method of claim 1 , wherein the boundaries of the shadow zone include at least one sloped zone to account for a parachute glide path of the balloon.