发明名称 FLASH LADAR SYSTEM
摘要 The present invention pertains in general to a single, integrated flash LADAR system and method. The system includes data processing hardware and software, a passive two-dimensional camera, a three-dimensional camera, a light source, and a common optical path. One or more star trackers can also be included. In addition, auxiliary components, such as an inertial measurement unit and a global positioning system receiver can be included. The system can be closely integrated with a critical algorithm suite that operates in multiple modes, in real-time to enable landing, docking, and navigation functions, such as Guidance, Navigation, and Control (GNC), Altimetry, Velocimetry, Terrain Relative Navigation (TRN), Hazard Detection and Avoidance (HDA), and dust penetration.
申请公布号 EP2429858(A4) 申请公布日期 2012.10.31
申请号 EP20100775273 申请日期 2010.05.04
申请人 BALL AEROSPACE & TECHNOLOGIES CORP. 发明人 EARHART, RONALD, P.;CRAIG, REX, M.;GRUND, CHRISTIAN, J.;GRAVSETH, IAN, J.;HUANG, XIAOPEI;WEIMER, CARL, S.
分类号 B60Q1/00;G01S3/786;G01S7/481;G01S17/02;G01S17/58;G01S17/87;G01S17/88;G01S17/89 主分类号 B60Q1/00
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