Patent ID: 9605934
Date: 2017-03-28
CPC Classifications: F41G,F42B,H03C

Claim:
1. A method of guiding a missile from a ground station, the missile including a missile body, the missile body and the ground station having respective up, down, left, and right directions, the missile body directions defined in the reference frame of the missile body, wherein the ground station includes an up transmitting antenna, a down transmitting antenna, a right transmitting antenna and a left transmitting antenna, the ground station antennas aligned with the ground station respective up, down, right and left directions, the method comprising: transmitting data from the ground station to the missile, the data including a value of the missile roll angle in a horizontal axis reference frame of the ground station; receiving the transmitted data on missile; and aligning the missile body up, down, left, and right directions with corresponding ground station up, down, left, and right directions according to the value in the received data.