2012•2012 IEEE/AIAA 31st Digital Avionics Systems Conference (DASC)Requires access

Fixed RTA fuel optimal profile descent based on analysis of trajectory performance bound

Sang Gyun Park, J. B. Clarke

Abstract

A collection of slides from the author's conference presentation is given. The following topics are discussed: TPA framework for obtaining trajectory performance bound of individual aircraft is proposed; fixed RTA suboptimal trajectory generation method is proposed; trajectory structure is designed by analysis of real optimal trajectory; and the suboptimal trajectory shows the similar performance comparing to real optimal trajectory.

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Available abstract

Key concepts: Trajectory, Descent (aeronautics), Computer science, Trajectory optimization, Mathematical optimization, Control theory (sociology), Mathematics, Engineering