System and method for drone release detection

1. A system comprising:

one or more Unmanned Aerial Vehicles (UAVs); and

a UAV carrier configured to carry the UAVs from an origin to a destination;

wherein the UAV carrier comprises a first controller configured to release the UAVs from the UAV carrier; and

wherein each of the UAVs comprises:

one or more motors configured to generate, directly or indirectly, a lift, lifting the UAV; and

a second controller, configured to:

activate at least one of the motors of the respective UAV after the release of the respective UAV from the UAV carrier and upon fulfilment of one or more conditions, thereby generating the lift, wherein the conditions include one or more of the following: (a) that each of the UAVs further comprises an accelerometer, and that readings of the accelerometer indicate that the respective UAV reaches a terminal velocity, (b) that each of the UAVs further comprises an altimeter, and that the readings of the altimeter indicate that the respective UAV reached a given altitude, (c) that each of the UAVs has an armed state and a disarmed state, and that the respective UAV is in the armed state, and (d) that each of the UAVs further comprises a distance sensor, capable of measuring a distance between the respective UAV and the UAV carrier, and that the readings of the distance sensor indicate that the respective UAV reached a given distance from the UAV carrier.

2. The system according to claim 1 , wherein at least one of the conditions is that a pre-determined time passed since the UAV was released from the UAV carrier.

3. The system according to claim 1 , wherein each of the UAVs further comprises a distance sensor, capable of measuring a distance between the UAV and the UAV carrier, and wherein at least one of the conditions is that the readings of the distance sensor indicate that the UAV reaches a given distance from the UAV carrier.

4. The system according to claim 1 , wherein each of the UAVs further comprises a mechanical safety catch, connected to a first end of a cable connected to the UAV carrier at a second end of the cable, so that the release of the respective UAV causes the cable to stretch and release the mechanical safety catch and wherein at least one of the conditions is that the mechanical safety catch is released.

5. The system according to claim 1 , wherein: (a) the UAVs are connected to the UAV carrier via one or more interface connections controlled by the first controller, (b) the UAVs are released by the first controller decoupling the interface connection, and (c) upon the interface connection being coupled the second controller prevents activation of the motors.

6. The system according to claim 1 , wherein the motors control respective rotors and wherein each of the UAVs further comprises a gyroscope, and wherein the second controller is configured to control the motors using gyroscope readings of the gyroscope, thereby enabling controlling at least one of a pitch angle, a roll angle or a yaw angle of the UAV.

7. A method comprising: carrying, by a UAV carrier, one or more Unmanned Aerial Vehicles (UAVs) from an origin to a destination; releasing, by a first controller of the UAV carrier, the UAVs from the UAV carrier; and for each UAV of the UAVs: activating, by a second controller of the respective UAV, at least one of the motors of the respective UAV, after the release of the respective UAV from the UAV carrier and upon fulfilment of one or more conditions, thereby generating, by one or more motors of the respective UAV, directly or indirectly, a lift, lifting the respective UAV; wherein the conditions include one or more of the following: (a) that each of the UAVs further comprises an accelerometer, and that readings of the accelerometer indicate that the respective UAV reaches a terminal velocity, (b) that each of the UAVs further comprises an altimeter, and that the readings of the altimeter indicate that the respective UAV reached a given altitude, (c) that each of the UAVs has an armed state and a disarmed state, and that the respective UAV is in the armed state, and (d) that each of the UAVs further comprises a distance sensor, capable of measuring a distance between the respective UAV and the UAV carrier, and that the readings of the distance sensor indicate that the respective UAV reached a given distance from the UAV carrier.

8. The method according to claim 7 , wherein at least one of the conditions is that a pre-determined time passed since the UAV was released from the UAV carrier.

9. The method according to claim 7 , wherein each of the UAVs further comprises a mechanical safety catch, connected to a first end of a cable connected to the UAV carrier at a second end of the cable, so that the release of the respective UAV causes the cable to stretch and release the mechanical safety catch and wherein at least one of the conditions is that the mechanical safety catch is released.

10. The method according to claim 7 , wherein: (a) the UAVs are connected to the UAV carrier via one or more interface connections controlled by the first controller, (b) the UAVs are released by the first controller decoupling the interface connection, and (c) upon the interface connection being coupled the second controller prevents activation of the motors.

11. A non-transitory computer readable storage medium having computer readable program code embodied therewith, the computer readable program code, executable by at least one processor of a computer to perform a method of: carrying, by a UAV carrier, one or more Unmanned Aerial Vehicles (UAVs) from an origin to a destination; releasing, by a first controller of the UAV carrier, the UAVs from the UAV carrier; and for each UAV of the UAVs: activating, by a second controller of the respective UAV, at least one of the motors of the respective UAV, after the release of the respective UAV from the UAV carrier and upon fulfilment of one or more conditions, thereby generating, by one or more motors of the respective UAV, directly or indirectly, a lift, lifting the respective UAV; wherein the conditions include one or more of the following: (a) that each of the UAVs further comprises an accelerometer, and that readings of the accelerometer indicate that the respective UAV reaches a terminal velocity, (b) that each of the UAVs further comprises an altimeter, and that the readings of the altimeter indicate that the respective UAV reached a given altitude, (c) that each of the UAVs has an armed state and a disarmed state, and that the respective UAV is in the armed state, and (d) that each of the UAVs further comprises a distance sensor, capable of measuring a distance between the respective UAV and the UAV carrier, and that the readings of the distance sensor indicate that the respective UAV reached a given distance from the UAV carrier.