发明名称 Spectral analyzer and direction indicator and aircraft landing system application
摘要 A spectral analyzer and direction indicator system (10) is disclosed and includes optical channels (20,30,40) for providing detected optical information indicative of incidence direction and spectral content of incident radiation. Each optical channel includes a reflector element (11,17,23) having a non-ruled section (11a,17a,23a) and a spectrally dispersing ruled section (11b,17b,23b); an analytical optical system (13,19,25); and a detector array (15,21,27). For each reflector element the non-ruled section is tilted in one or two directions relative to the ruled section. The disclosed spectral analyzer and direction indicator system is advantageously utilized as an aircraft based sensor in an aircraft landing system having ground lasers (29L,29R,33L,33R,37L,37R) directed into the landing approach path.
申请公布号 US4966456(A) 申请公布日期 1990.10.30
申请号 US19890374206 申请日期 1989.06.30
申请人 HUGHES AIRCRAFT COMPANY 发明人 SHIFRIN, GORDON A.
分类号 B64F1/20;G01J3/28;G01J9/00;G01S1/70;G01S3/784 主分类号 B64F1/20
代理机构 代理人
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