发明公开
- 专利标题: VERFAHREN UND VORRICHTUNG ZUM ERKENNEN VON KURSÄNDERUNGEN UND/ODER GESCHWINDIGKEITSÄNDERUNGEN EINES ZIELS
- 专利标题(英): Method and apparatus for identifying changes of course and/or changes of speed for a destination
- 专利标题(中): 用于识别过程变化和/或速度的方法和装置改变目的地
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申请号: EP10712310.1申请日: 2010-02-22
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公开(公告)号: EP2539738A1公开(公告)日: 2013-01-02
- 发明人: STEINER, Hans-Joachim , STEIMEL, Ulrich
- 申请人: ATLAS Elektronik GmbH
- 申请人地址: Sebaldsbrücker Heerstrasse 235 28309 Bremen DE
- 专利权人: ATLAS Elektronik GmbH
- 当前专利权人: ATLAS Elektronik GmbH
- 当前专利权人地址: Sebaldsbrücker Heerstrasse 235 28309 Bremen DE
- 代理机构: Wasiljeff, Johannes M.B.
- 国际公布: WO2011100938 20110825
- 主分类号: G01S15/58
- IPC分类号: G01S15/58 ; G01S3/808
摘要:
The invention relates to a method for identifying changes of course and/or speed for a destination using a multiplicity of measured bearing angles (22) which are ascertained by virtue of the directionally selective reception of sound waves emitted from the destination using an arrangement of water borne sound pickups (86) in a sonar receiving installation. To this end, a first bearing profile (40) is calculated from a predetermined number k of most recently ascertained bearing angles, and a second bearing profile (42) is calculated from a predetermined number i of earlier bearing angles ascertained before the k bearing angles. An expected bearing angle (56, 58) for each of the two bearing profiles (40, 42) is calculated at a current time (54) and is used to form a bearing angle difference |
d |. This bearing angle difference |
d | can be compared with a plurality of threshold values C1, C2, wherein an intersection point (72) for the bearing profiles (40, 42) and an associated target manoeuvre time (74) are ascertained when one of the threshold values C1, C2 is reached and are output together with an information signal (75) relating to the identification of the target manoeuvre. The invention also relates to an apparatus for carrying out such a method.
d |. This bearing angle difference |
d | can be compared with a plurality of threshold values C1, C2, wherein an intersection point (72) for the bearing profiles (40, 42) and an associated target manoeuvre time (74) are ascertained when one of the threshold values C1, C2 is reached and are output together with an information signal (75) relating to the identification of the target manoeuvre. The invention also relates to an apparatus for carrying out such a method.
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