发明名称 Method and apparatus for limiting attitude drift during turns
摘要 An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information. During bank angles exceeding a predefined limit, the roll gyro is slaved to a roll angle estimator for improved system accuracy.
申请公布号 US6456905(B2) 申请公布日期 2002.09.24
申请号 US20000746128 申请日期 2000.12.22
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 KATZ KENNETH P.;LEHFELDT JAMES J.;OBERG JOSEPH M.;SAMPLE WILLIAM G.;WILSON RONALD D.
分类号 G01C19/30;G01C21/16;(IPC1-7):G06F1/00 主分类号 G01C19/30
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