发明名称 DECELERATION SCHEDULE FOR AIRCRAFT LANDING
摘要 An aircraft guidance system for generating a speed reduction schedule during deceleration along a known descent angle. Radar-sensed altitude along the descent angle is used to produce a signal representative of the aircraft's range to touchdown. The derived range signal is used to command a controlled speed reduction as range to touchdown decreases.
申请公布号 US3665465(A) 申请公布日期 1972.05.23
申请号 USD3665465 申请日期 1969.10.22
申请人 RITA ANN MILLER;LEAR-SIEGLER INC. 发明人 JUSTIN G. MILLER
分类号 G05D1/06;(IPC1-7):B64C19/00 主分类号 G05D1/06
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