发明名称 SYSTEM AND METHOD FOR SIMULATING AIR MODE AND GROUND MODE OFAN AIRPLANE
摘要 A system for simulating an air mode and a ground mode of an airplane is provided. The air mode is a state of the airplane when the airplane is in the ai r, and the ground mode is a state of the airplane when the airplane is on the ground. The s ystem includes means for sensing parameters indicative of whether the airplane is sens ed in the air or sensed on the ground. Means for determining whether the airplane is sense d in the air or sensed on the ground is provided. The determining means is responsive to the sensing means, and the determining means outputs a signal that is indicative of a sensed air mode or a sensed ground mode. Means for interfacing with an operator is also provided. A simulated air mode and a simulated ground mode are selectable via th e interface means. Means for overriding the signal output from the determining mea ns is provided, and the overriding means outputs a signal that is indicative of the si mulated air mode or the simulated ground mode in response to a selection from the interf ace means. The overriding means outputs a signal that is indicative of the sensed ai r mode or the sensed ground mode when the simulated air mode or the simulated ground mo de is not selected.
申请公布号 CA2253733(A1) 申请公布日期 1999.05.10
申请号 CA19982253733 申请日期 1998.11.10
申请人 THE BOEING COMPANY 发明人 GUNDERSON, DENIS P.;BROUWER, TODD B.;MOLSBERRY, LAUNA B.
分类号 G09B9/08;(IPC1-7):G09B9/08 主分类号 G09B9/08
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