|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-013/00 B64D-039/00 G05D-001/08 G05D-001/06|
|우선권정보||FR-14 57145 (2014-07-24)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 5|
The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.
1. An automated method performed by a control system to control the amount of lift produced during flight of an aircraft in response to a control signal received in response to a manual activation of a control column of the aircraft by a pilot, wherein the aircraft comprises at least one elevator and at least one lift generator that directly modifies the amount of lift produced during flight and that is a separate control surface from the at least one elevator, the method comprising: extracting, by the control system, a limited portion of the control sig...