|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 17|
Technologies are described herein for providing additional yaw control to a multi-engine aircraft experiencing engine thrust asymmetry. A primary flight control system of the aircraft is configured to limit the operational thrust of an operating engine of the aircraft to provide additional yaw control when the aircraft is experiencing thrust asymmetry. The system includes a thrust limit module for calculating the maximum engine thrust limit to be imposed on an operating engine. The maximum engine thrust limit is calculated using inputs corresponding to t...
1. A method for providing additional yaw control to a multi-engine aircraft experiencing thrust asymmetry, comprising: receiving an aircraft sideslip input corresponding to an aircraft sideslip angle of the aircraft;receiving an aircraft roll input corresponding to at least one of an aircraft roll command and an aircraft roll rate;calculating a maximum engine thrust limit with a primary flight control system of the multi-engine aircraft using the aircraft sideslip input and the aircraft roll input and a reference engine thrust value;determining with the ...