Fire control device for, in particular, transportable air defense systems
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41G-005/18
F41G-003/18
G06F-019/00
출원번호
US-0348560
(1994-03-03)
우선권정보
DE-4306913 (1993-03-05)
발명자
/ 주소
Ennenga Luitjen,DEX
출원인 / 주소
STN Atlas Elektronic GmbH, DEX
대리인 / 주소
VenableKunitz
인용정보
피인용 횟수 :
13인용 특허 :
3
초록▼
A fire-control system for anti-aircraft defense systems, particularly mobile ones, having at least one launch apparatus for guided missiles that is pivotable in elevation and disposed on a platform that is pivotable in azimuth, has an optical target-tracking sensor that is rigidly coupled with the l
A fire-control system for anti-aircraft defense systems, particularly mobile ones, having at least one launch apparatus for guided missiles that is pivotable in elevation and disposed on a platform that is pivotable in azimuth, has an optical target-tracking sensor that is rigidly coupled with the launch apparatus, a follow-up computer for panning the target-tracking sensor after targets, a directional angle computer for calculating lead and elevation of the guided missile during launch, and a control unit that has adjustment drives for the platform and launch apparatus, which unit pivots the platform in azimuth and the launch apparatus in elevation, and, prior to launch, locks the lead on the platform and the elevation on the launch apparatus. For the purpose of a very rapid second attack, the line of sight of the target-tracking sensor rigidly coupled with the launch apparatus is guided via a vertically and horizontally pivotable pivoting mirror that is positioned during lock-on of lead and elevation by azimuth and elevation angles that correspond to those for the platform and launch apparatus, but in a direction counter to the direction of displacement of the platform and launch apparatus.
대표청구항▼
[ What is claimed is:] [1.] A fire-control apparatus for anti-aircraft defense systems comprising: a platform that rotates around a vertical axis; at least one launch apparatus for guided missiles equipped with homing heads, which apparatus is pivotable around a horizontal axis and is disposed on th
[ What is claimed is:] [1.] A fire-control apparatus for anti-aircraft defense systems comprising: a platform that rotates around a vertical axis; at least one launch apparatus for guided missiles equipped with homing heads, which apparatus is pivotable around a horizontal axis and is disposed on the platform; at least one optical target-tracking sensor which continuously determines target position, velocity and range data, rigidly coupled with the launch apparatuses; a directional angle computer that is connected to the target-tracking sensor and, from the target data, calculates the estimated point of impact of a guided missile and an airborne target and the directional angles "lead" and "elevation" necessary for the launch of the guided missile; a follow-up computer that is connected to the target-tracking sensor and generates follow-up signals in azimuth and elevation from the deviations of the target position from the line of sight of the target-tracking sensor; a control unit, connected to the follow-up and directional angle computers and having adjustment drives for the platform and launch apparatus, which pivots the platform in azimuth and the launch apparatuses in elevation as a function of the follow-up signals, and which, directly prior to launch and in response to a launch signal, locks the lead on the platform and the elevation on the launch apparatus; a vertically and horizontally pivotable pivoting mirror for guiding the line of sight of the target-tracking sensor; and a mirror drive that drives the pivoting mirror and is controlled by the control unit such that the pivoting mirror is adjusted, prior to launch and during the time the lead on the platform and the elevation on the launch apparatus are locked on, in lead and elevation by an azimuth angle (.alpha.) and an elevation angle (.epsilon.) corresponding to but counter to the direction of adjustment of the platform and the launch apparatus.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (3)
Alston Steven C. (Bonney Lake WA) Hack Kenneth W. (Seattle WA) Hibbert John A. (Federal Way WA), Automatic turret tracking apparatus for a light air defense system.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.