摘要 |
The present invention is a method and system of aircraft surface operations guidance on a head up display. An aircraft surface operations guidance method includes the following steps. At time t<SUB>1</SUB>, a taxi guidance cue and a trend vector are displayed on a head up display of an aircraft. The taxi guidance cue represents a desired position of an aircraft control point of the aircraft at time t<SUB>2</SUB>. The trend vector represents a predicted path of the aircraft control point from time t<SUB>1 </SUB>to time t<SUB>2 </SUB>based on a state of the aircraft at time t<SUB>1</SUB>. The trend vector includes a tip representing a predicted position of the aircraft control point at time t<SUB>2</SUB>. The tip is maintained within the taxi guidance cue so that the aircraft control point may reach the desired position at time t<SUB>2</SUB>.
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