|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-013/08 B64C-013/50 G05D-001/00|
|미국특허분류(USC)||244/220; 244/175; 244/235|
|우선권정보||FR-11 58550 (2011-09-26)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 4|
Disclosed is a vertical rudder control system for an aircraft. The system is comprised of a rudder trim compensation generator that is configured to generate a rudder trim compensation order to set the position of the rudder bar of the aircraft to a neutral position in which the rudder bar is controlled with nil (i.e., zero) pilot effort. The vertical rudder control system includes a flight control calculator for calculating rudder control orders to maintain the nil effort rudder bar position, with the calculation of the rudder control orders being based...
1. A vertical rudder control system for an aircraft, comprising: a rudder bar configured for actuation by a pilot of said aircraft;rudder bar position detection unit configured for detecting rudder bar position and generating an electrical control signal corresponding to the rudder bar position;rudder trim compensation generator for generating a rudder trim compensation order setting a nil effort rudder bar position as a rudder bar neutral position, wherein the rudder bar compensation generator generates an auxiliary electrical signal based on the genera...