System and method of providing a cocklebur net in a projectile module
A projectile component that can be removably attached to a flying vehicle is disclosed. The projectile component includes a net configured in the projectile component, a receiving cavity configured in the projectile component, and a weight attached to the net via a string. The weight can be configured in the receiving cavity in preparation for firing the net from the projectile component. In order to entangle a target flying vehicle in the net, a cocklebur associated with the weight is included. Upon firing the net from the projectile component, and upon the net engaging with a target device, the cocklebur becomes entangled with the net to secure the target flying vehicle. A drawstring structure associated with the net can also be used to ensure that the net envelops and captures the target flying vehicle.
1. A flying vehicle comprising:
a processor;
a projectile component;
a net configured in the projectile component, the net comprising a cocklebur; and
a non-transitory computer-readable storage medium storing instructions which, when executed by the processor, cause the processor to perform operations comprising:
receiving an identification of a target flying device;
applying a projectile model which generates a determination which indicates whether the net, if fired from the projectile component, will hit the target flying device, the projectile model taking into account one or more of a wind modeling in an area around the flying vehicle based on an inference of wind due to a tilt of the flying vehicle and a projected movement of the target flying device based on the identification of the target flying device; and
when the determination indicates that the net will hit the target flying device according to a threshold value, firing the net at the targeted flying device, wherein the cocklebur is configured to become entangled with the net upon interaction of the net with the target flying device.
2. The flying vehicle of claim 1 , wherein the cocklebur comprises a first cocklebur and wherein the net further comprises:
a first weight attached to a first location of the net via a first string, wherein the first cocklebur is configured on the first string that attaches the first weight to the first location of the net;
a second weight attached to a second location of the net via a second string; and
a second cocklebur configured on the second string that attaches the second weight to the second location of the net.
3. The flying vehicle of claim 2 , wherein the net further comprises:
a third weight attached to a third location of the net via a third string;
a third cocklebur configured on the third string that attaches the third weight to the third location of the net;
a fourth weight attached to a fourth location of the net via a fourth string; and
a fourth cocklebur configured on the fourth string that attaches the fourth weight to the fourth location of the net.
4. The flying vehicle of claim 3 , wherein the net further comprises:
a fifth cocklebur on a fifth string, the fifth string being attached to a first side of the net;
a sixth cocklebur on a sixth string, the sixth string being attached to a second side of the net;
a seventh cocklebur on a seventh string, the seventh string being attached to a third side of the net; and
an eighth cocklebur on an eighth string, the eighth string being attached to a fourth side of the net.
5. The flying vehicle of claim 1 , further comprising:
a weight connected to the net, wherein the projectile component comprises a first receiving cavity that receives the weight in preparation for firing the net.
6. The flying vehicle of claim 1 , further comprising a tether connecting the net to the flying vehicle.
7. The flying vehicle of claim 1 , wherein the cocklebur is configured on a weight that is attached to the net.
8. The flying vehicle of claim 1 , further comprising:
a first weight connected to the net, the first weight being associated with the cocklebur;
a second weight connected to the net, the second weight being associated with a second cocklebur;
a third weight connected to the net, the third weight being associated with a third cocklebur; and
a fourth weight connected to the net, the fourth weight being associated with a fourth cocklebur, wherein each of the first weight, the second weight, the third weight and the fourth weight are configured in a respective receiving cavity of the projectile component in preparation for firing the net.
9. The flying vehicle of claim 8 , wherein the cocklebur, the second cocklebur, the third cocklebur and the fourth cocklebur are each configured, in preparation for firing, in one of the respective receiving cavity with its associated respective weight or on an exterior surface of a breakable covering configured over the net in the projective component.
10. The flying vehicle of claim 8 , wherein the cocklebur is connected to the first weight, the second cocklebur is connected to the second weight, the third cocklebur is connected to the third weight and the fourth cocklebur is connected to the fourth weight.
11. The flying vehicle of claim 1 , further comprising:
a first weight connected to a location of the net via a string, wherein the cocklebur is configured on the string;
a second weight connected to the location of the net via a second string; and
a second cocklebur configured on the second string.
12. The flying vehicle of claim 11 , further comprising:
a third weight connected to the location of the net via a third string; and
a third cocklebur configured on the third string.
13. The flying vehicle of claim 1 , wherein:
the cocklebur is attached to a weight; and
the weight is attached to the net via a string.
14. The flying vehicle of claim 13 , further comprising:
a grappling hook configured with the weight; and
a spring configured with the grappling hook to deploy the grappling hook from the weight upon the projectile component firing the net.
15. A flying vehicle comprising:
a processor;
a projectile component;
a net configured in the projectile component;
a first weight attached to a first location of the net;
a second weight attached to a second location of the net;
a first cocklebur, wherein the first cocklebur is attached to the first weight or is attached to the net at a first location, wherein the first location is not at a corner of the net;
a second cocklebur, wherein the second cocklebur is attached to the second weight or is attached to the net at a second location, wherein the second location is not at the corner of the net; and
a non-transitory computer-readable storage medium storing instructions which, when executed by the processor, cause the processor to perform operations comprising:
receiving an identification of a target flying device; and
firing the net from the projectile component, wherein the cocklebur is configured to become entangled with the net upon interaction of the net with the target flying device.
16. The flying vehicle of claim 15 , further comprising a tether connecting the net to the flying vehicle.
17. The flying vehicle of claim 16 , further comprising:
a tether release controller, wherein the tether release controller that holds or releases the tether based on one or more criteria.
18. The flying vehicle of claim 17 , wherein the one or more criteria comprises one or more of an angle of the tether towing a captured target flying device, a force on the tether associated with a weight of the captured device, a timing factor, an energy parameter associated with battery power and a priority criteria.