Invention Grant
US07095488B2 System for profiling objects on terrain forward and below an aircraft utilizing a cross-track laser altimeter
失效
用于使用跨轨道激光高度计对飞机前方和下方的地形进行分析的系统
- Patent Title: System for profiling objects on terrain forward and below an aircraft utilizing a cross-track laser altimeter
- Patent Title (中): 用于使用跨轨道激光高度计对飞机前方和下方的地形进行分析的系统
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Application No.: US10347908Application Date: 2003-01-21
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Publication No.: US07095488B2Publication Date: 2006-08-22
- Inventor: James R. Jamieson , Mark D. Ray , Joseph T. Pesik
- Applicant: James R. Jamieson , Mark D. Ray , Joseph T. Pesik
- Applicant Address: US MN Burnsville
- Assignee: Rosemount Aerospace Inc.
- Current Assignee: Rosemount Aerospace Inc.
- Current Assignee Address: US MN Burnsville
- Agency: Calfee, Halter & Griswold LLP
- Agent James M. Rashid, Esq.
- Main IPC: G01C3/08
- IPC: G01C3/08 ; G01C1/00 ; G01B11/26

Abstract:
A forward looking cross-track laser altimeter comprises: a first configuration of optical elements for guiding pulsed laser beams along a first optical path; a mirror element coupled to a scanner and disposed in the first optical path, the scanner operative to oscillate the mirror element to sweep the reflected laser beams back and forth across a line at a predetermined frequency; the scanner and mirror element configurable to reflect the pulsed laser beams along paths forward and downward at a predetermined angle to the flight path of the aircraft, wherein the pulsed laser beam paths are caused to be line swept across a ground track forward the aircraft; the mirror element for receiving returns of the pulsed laser beams from the terrain and objects on the terrain forward the aircraft and reflecting the returns along a second optical path to a light detector which produces a return signal in response thereto; a first circuit governed by the return signals for measuring times-of-flight of the returns and generating time-of-flight signals corresponding thereto; the scanner for generating a line sweep position signal; and a second circuit for generating for each return a data profile comprising range and line sweep position thereof based on the corresponding time-of-flight and position signals.
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