Patent ID: 9033281
Filing Date: 2015-05-19
Classification: B64C,B64D

Abstract:
1. An unmanned aerial reconnaissance vehicle (UAV) system comprising: a parachute having a plurality of control lines comprising at least one first control line attached to one portion of said parachute and at least one second control line attached to another portion of said parachute, said parachute configured to be steered by simultaneous vertical movement of said at least one first control line and said at least one second control line, a power and control module of an elongated, generally cylindrical configuration suspended in a vertical orientation below said parachute, said power and control module further comprising: a signal receiver in said power and control module, a control mechanism attached to said at least one first control line and said at least one second control line, said control mechanism responsive to signals received by said signal receiver to move said at least one first control line and said at least one second control line in said simultaneous vertical movement, for controlling direction of said parachute, and a remote controller that transmits said signals to a flying said UAV.