发明名称 IMPROVED AIRCRAFT INSTRUMENT FLIGHT DISPLAY SYSTEM WITH INTEGRITY OF GRAPHIC IMAGE
摘要 PROBLEM TO BE SOLVED: To provide an integrity checking function and the graphics rendering function to an aircraft instrument flight display system for imaging aircraft flight information by the bit map display. SOLUTION: A common processor 216 for operably connecting a common set of the aircraft and environmental sensor data 214 to a video graphics processor 206 is employed. The bit map display is individually addressible, and formed of a plurality of pixels. An integrity checking function 202 can directly check the image generated by the graphics rendering function 204. A separate processor can also be used in place of the common processor. The integrity checking function uses information input for generating the pixel verification map for checking the display based on the pixel color and position. The system can check the pitch and the roll accuracy in addition to the checking of a complicated image by using the statistical checking. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2007055587(A) 申请公布日期 2007.03.08
申请号 JP20060194515 申请日期 2006.07.14
申请人 INNOVATIVE SOLUTIONS & SUPPORT INC 发明人 HEDRICK GEOFFREY S M;ASKARPOUR SHAHRAM;KNOPF MARKUS;COLLINS JEFF
分类号 B64D45/00;G08G5/00 主分类号 B64D45/00
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