|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/42406 ; 364/183 ; 364/424013 ; 364/553|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 11|
A method and system for controlling transitions between attitude command/response and rate command/response in an aircraft control system wherein the transfer function for a generic second order system is developed at current operating conditions and a predetermined constant damping. During a transition, trim follow-up frequency is changed progressively to coincide with the desired bandwidth, thereby effecting a pole-zero cancellation and converting the transfer function to that of a rate command/response system. Actuators, responsive to signals produced...
A method for switching between command/response modes in a flight control system that controls the magnitude of an aircraft parameter, the method comprising the steps of: producing a command representing a desired change in magnitude of the parameter; determining whether the desired response to the command is to be provided by a control system characterized by a second order transfer function or by a control system characterized by a first order transfer function; developing a first transfer function for a dynamic system of second order having poles at a...