INTEGRATED FLIGHT MANAGEMENT SYSTEM AND FLIGHT DIRECTOR

摘要

Systems and methods for controlling an aerial vehicle (100) are provided. Themethod includes receiving a first signal from a first input device (202),wherein the firstsignal is related to a mode of a flight director (116). The method includesoutputting aparameter on an output device (206), wherein the parameter is related to themode. Themethod includes receiving a second signal from a second input device (208),wherein thesecond signal causes the parameter to change to a new parameter. The methodincludesoutputting, by the one or more processors (404), the new parameter on theoutput device(206). The method includes receiving, by the one or more processors (404), athird signalfrom a third input device (210), wherein the aerial vehicle (100) iscontrolled by the flightdirector (116) based on the third signal, and wherein the second input device(208) ismechanically coupled to the first input device (202) and the third inputdevice (210).