|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F41G-007/20 F42B-010/64 F42B-010/34|
|미국특허분류(USC)||244/311 ; 244/321 ; 244/324 ; 102/384|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 34 인용 특허 : 0|
An artillery rocket including a motor for the launching thereof into a ballistic trajectory across a specified target area over which a payload is to be released. The rocket is equipped with a flight controller or autopilot for the control over a rudder or control surface-setting or control system which is actuatable from a navigational receiver with actual positional coordinates. The flight controller operates on a control or setting system which is disposed in front of the warhead in the forward region of the nose cone without noticeably restricting th...
An artillery rocket including a warhead carrying a payload; a motor for launching said rocket into a ballistic trajectory above a specified target area over which the payload is to be released, said rocket comprising a flight controller for the control of a control system for a plurality of canard control surfaces; a navigational receiver with actual positional coordinates for actuating said flight controller; said flight controller, said control system for the control surfaces, said navigational receiver, a roll-position sensor, and a power supply being...