Patent ID: 8963742
Filing Date: 2015-02-24
Classification: G01C,G08G

Abstract:
1. A system, comprising: an aircraft, including at least one sensor configured to detect information about at least one state parameter of a present position of the aircraft; a head-up display, comprising: wherein the graphical display includes a three-dimensional graphical representation of the predicted trajectory and the predicted trajectory includes one or more predicted locations for the aircraft at one or more future times different than a current time at which the predicted trajectory is displayed, the at least one state parameter of the present position of the aircraft includes a second order derivative of a state of the aircraft and the predicted trajectory for the aircraft over a period of time based on the at least one state parameter, the predicted flight path generation component uses a predicted first order derivative of the state of the aircraft based upon the second order derivative to refine the one or more predicted locations for the aircraft at the one or more future times.