Technologically improved flight guidance systems and methods that generate thrust guidance related to a potential flight path angle are provided. The thrust guidance is provided as acceleration commands that may be communicated to the pilot in an intuitive manner, such as with an acceleration cue on a primary flight display (PFD) system. The provided acceleration cues are uniform across the flight envelope and present consistently for two basic thrust guidance modes.
Systems and methods for providing thrust guidance related to flight path angle
2021-09-14
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR PROVIDING THRUST GUIDANCE RELATED TO FLIGHT PATH ANGLE
European Patent Office | 2021
|SYSTEMS AND METHODS FOR PROVIDING THRUST GUIDANCE RELATED TO FLIGHT PATH ANGLE
European Patent Office | 2021
|SYSTEMS AND METHODS FOR ENERGY MANAGED AUTOFLIGHT GUIDANCE USING POTENTIAL FLIGHT PATH ANGLE
European Patent Office | 2021
|Flight-Path Angle Control for Cutoff Insensitive Guidance
Online Contents | 2015
|