|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/090R; 244/194; 244/045A|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 13 인용 특허 : 30|
Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes thrusters mounted to an aircraft, a first control surface kinematically coupled to the aircraft downstream of a first thruster to enable a first vector force to be generated by a portion of thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft of a second thruster. The control surface...
1. A method for configuring an attitude control for an aircraft comprising: kinematically coupling a first control surface and a second control surface to an aircraft so the first and the second control surfaces are differentially moveable; andmounting a thruster to the aircraft at a position that enables thrusted air from the thruster to generate a first vector force on the first control surface, a second vector force generated by thrusted air on the second control surface, so that the first and the second vector forces provide a net roll moment about t...