|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/003.13; 244/003.11; 244/003.14; 244/003.15; 244/003.16; 244/003.19|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 20 인용 특허 : 13|
The present invention relates to a method and an arrangement for guiding a missile. In accordance with the prior art, the angle position of a target (9) when the missile (3) is expected to reach the target is predicted on the basis of the angular velocity determined in a preceding time period. In order to improve the strike accuracy, the operator, in a second subsequent time period, tracks the actual position of the missile in relation to the predicted angle position of the target. If a deviation is observed, a correction command is transmitted to the mi...
1. A method for guiding a missile fired at a target, the method comprising: tracking the target in a first time period to determine an angular velocity of the target, the tracking including recording at least a first angle position and a second angle position and a time interval between the first angle position and the second angle position; predicting an assumed angle position that the target is assumed to have when the missile reaches the target based on the determined angular velocity; continuously guiding the missile in a trajectory towards the ...