|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/463 ; 73/65|
|§371/§102 date||19880812 (19880812)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 24 인용 특허 : 4|
Method and system for determining the longitudinal position of the gravity center of an aircraft having an adjustable stabilizer. At a flight point for which the aircraft is in equilibrium with its elevator in aerodynamic prolongation of the adjustable stabilizer, the gravity center position is calculated from the position (XF) of the focus (F) of the aircraft (1), the measurement of the deflection (iH) of the adjustable stabilizer, a first function K(M, N1) of the engine speed (N1) of the engines of the aircraft and the Mach number (M). The first functi...
A system for determining the longitudinal position XG of the center of gravity G of an aircraft in flight, said aircraft being provided with an adjustable horizontal stabilizer which is deflectable and to which is articulated an elevator, said aircraft having a determined focus F with a longitudinal position XF, speed of engine, Mach number and coefficient of lift, said system comprising: means for transferring fuel from one tank of the aircraft to another; angular position sensing means associated with said adjustable horizontal stabilizer for measuring...