A system, comprising: an aircraft, comprising: at least one rotor having rotor blades; a phased array configured to at least one of transmit electromagnetic energy in a direction toward the rotor blades or receive EM energy in a direction from the rotor blades; and at least one processor communicatively coupled to the phased array, the at least one processor configured to: at least one of determine or obtain rotor blade information, the rotor blade information including at least one location of the rotor blades; at least one of determine or obtain aircraft information, the aircraft information including a position and an orientation of the aircraft; based at least on the rotor blade information and the aircraft information, determine (a) at least one time to at least one of transmit EM energy or receive EM energy and (b) at least one angle to at least one of transmit EM energy or receive EM energy; and based at least on the rotor blade information and the aircraft information, control the phased array to adjust at least one beam pointing angle of the phased array to one or more of the at least one angle and to transmit EM energy for a particular duration at the at least one adjusted beam pointing angle; wherein the phased array is configured to transmit EM energy for the particular duration at the at least one adjusted beam pointing angle, wherein the transmitted EM energy is configured to reflect off at least one of the rotor blades toward at least one target; wherein the at least one processor is further configured to determine whether to-be-transmitted or to-be-received EM energy is to dodge the rotor blades or to reflect off at least one of the rotor blades; and wherein the at least one processor is further configured to determine that to-be-transmitted or to-be-received EM energy is to dodge the rotor blades. at least one rotor having rotor blades; a phased array configured to at least one of transmit electromagnetic energy in a direction toward the rotor blades or receive EM energy in a direction from the rotor blades; and at least one processor communicatively coupled to the phased array, the at least one processor configured to: at least one of determine or obtain rotor blade information, the rotor blade information including at least one location of the rotor blades; at least one of determine or obtain aircraft information, the aircraft information including a position and an orientation of the aircraft; based at least on the rotor blade information and the aircraft information, determine (a) at least one time to at least one of transmit EM energy or receive EM energy and (b) at least one angle to at least one of transmit EM energy or receive EM energy; and based at least on the rotor blade information and the aircraft information, control the phased array to adjust at least one beam pointing angle of the phased array to one or more of the at least one angle and to transmit EM energy for a particular duration at the at least one adjusted beam pointing angle; wherein the phased array is configured to transmit EM energy for the particular duration at the at least one adjusted beam pointing angle, wherein the transmitted EM energy is configured to reflect off at least one of the rotor blades toward at least one target; wherein the at least one processor is further configured to determine whether to-be-transmitted or to-be-received EM energy is to dodge the rotor blades or to reflect off at least one of the rotor blades; and wherein the at least one processor is further configured to determine that to-be-transmitted or to-be-received EM energy is to dodge the rotor blades. at least one of determine or obtain rotor blade information, the rotor blade information including at least one location of the rotor blades; at least one of determine or obtain aircraft information, the aircraft information including a position and an orientation of the aircraft; based at least on the rotor blade information and the aircraft information, determine (a) at least one time to at least one of transmit EM energy or receive EM energy and (b) at least one angle to at least one of transmit EM energy or receive EM energy; and based at least on the rotor blade information and the aircraft information, control the phased array to adjust at least one beam pointing angle of the phased array to one or more of the at least one angle and to transmit EM energy for a particular duration at the at least one adjusted beam pointing angle; wherein the phased array is configured to transmit EM energy for the particular duration at the at least one adjusted beam pointing angle, wherein the transmitted EM energy is configured to reflect off at least one of the rotor blades toward at least one target; wherein the at least one processor is further configured to determine whether to-be-transmitted or to-be-received EM energy is to dodge the rotor blades or to reflect off at least one of the rotor blades; and wherein the at least one processor is further configured to determine that to-be-transmitted or to-be-received EM energy is to dodge the rotor blades.