An aerial vehicle securing system for use with a base portion (12, 112) of an aerial vehicle (10, 110), comprising: at least one flat platform for supporting said base portion upon landing of the aerial vehicle thereon; at least one magnetizable element (16, 116) configured to be integrated in said base portion; the aerial vehicle securing system being characterized in that it comprises: at least one electropermanent magnet configured to be integrated in said platform, said electropermanent magnet constituting a majority of an upper flat surface of said platform and defining a contact surface larger than a contact surface of said at least one magnetizable element, said electropermanent magnet comprising at least two sections, one of high coercivity permanent magnetic material and another one of low coercivity permanent magnetic material, the at least two sections being configured for selectively generating and cancelling a net magnetic field of the electropermanent magnet in response to an electric pulse of current and maintaining said net magnetic field in the absence of said electric pulse of current, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the aerial vehicle on the platform, said net magnetic field is configured to cause said at least one magnetizable element to be attracted to said at least one electropermanent magnet; a power supply module configured for generating said electric pulse of current to said at least one electropermanent magnet for selectively generating and cancelling said net magnetic field, wherein at least one of the at least two sections is configured for changing a direction of its magnetization in response to said electric pulse of current, thereby selectively generating and cancelling said net magnetic field; and a controlling module configured for controlling supply of said electric pulse of current. at least one flat platform for supporting said base portion upon landing of the aerial vehicle thereon; at least one magnetizable element (16, 116) configured to be integrated in said base portion; the aerial vehicle securing system being characterized in that it comprises: at least one electropermanent magnet configured to be integrated in said platform, said electropermanent magnet constituting a majority of an upper flat surface of said platform and defining a contact surface larger than a contact surface of said at least one magnetizable element, said electropermanent magnet comprising at least two sections, one of high coercivity permanent magnetic material and another one of low coercivity permanent magnetic material, the at least two sections being configured for selectively generating and cancelling a net magnetic field of the electropermanent magnet in response to an electric pulse of current and maintaining said net magnetic field in the absence of said electric pulse of current, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the aerial vehicle on the platform, said net magnetic field is configured to cause said at least one magnetizable element to be attracted to said at least one electropermanent magnet; a power supply module configured for generating said electric pulse of current to said at least one electropermanent magnet for selectively generating and cancelling said net magnetic field, wherein at least one of the at least two sections is configured for changing a direction of its magnetization in response to said electric pulse of current, thereby selectively generating and cancelling said net magnetic field; and a controlling module configured for controlling supply of said electric pulse of current. at least one electropermanent magnet configured to be integrated in said platform, said electropermanent magnet constituting a majority of an upper flat surface of said platform and defining a contact surface larger than a contact surface of said at least one magnetizable element, said electropermanent magnet comprising at least two sections, one of high coercivity permanent magnetic material and another one of low coercivity permanent magnetic material, the at least two sections being configured for selectively generating and cancelling a net magnetic field of the electropermanent magnet in response to an electric pulse of current and maintaining said net magnetic field in the absence of said electric pulse of current, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the aerial vehicle on the platform, said net magnetic field is configured to cause said at least one magnetizable element to be attracted to said at least one electropermanent magnet; a power supply module configured for generating said electric pulse of current to said at least one electropermanent magnet for selectively generating and cancelling said net magnetic field, wherein at least one of the at least two sections is configured for changing a direction of its magnetization in response to said electric pulse of current, thereby selectively generating and cancelling said net magnetic field; and a controlling module configured for controlling supply of said electric pulse of current.