发明名称 Warning system for tactical rotary wing aircraft
摘要 A warning system for rotary wing aircraft that monitors the altitude above ground of the aircraft and issues a warning when there is insufficient terrain clearance. The warning criteria are optimized for rotary wing aircraft and are altered as a function of landing gear position and airspeed. Two distinct warnings are given. One indicates insufficient terrain clearance and the other warns the pilot if he attempts to land with the landing gear up. Logic circuitry is provided to modify the criteria necessary to generate a warning, and to inhibit certain warnings, as required by the mode of operation of the aircraft.
申请公布号 US4980684(A) 申请公布日期 1990.12.25
申请号 US19840629607 申请日期 1984.07.11
申请人 SUNDSTRAND DATA CONTROLS, INC. 发明人 PATERSON, NOEL S.;GLOVER, JOHN H.
分类号 G01C5/00 主分类号 G01C5/00
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