|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/463; 235/061.T; 073/065|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 7 인용 특허 : 2|
In order to determine the location of the center of gravity of an aircraft in flight, an accelerometer is placed in the forward part of the aircraft and another is placed in the after part to produce signals representing the rotation of aircraft about an axis, preferably the yaw axis, through the aircraft center of gravity. The signals from the accelerometers are combined to produce a first signal having components that represent both motion of the aircraft and the location of the center of gravity along with a signal having a component representing the ...
1. An aircraft in flight center of gravity measuring system comprising: a pair of inertial sensors secured to the aircraft, each inertial sensor having a sensitive axis which is aligned so as to produce a signal representing the rotation of the aircraft about a predetermined axis through the aircraft center of gravity; and signal processing means connected to said inertial sensors including means for developing a signal from the output of the inertial sensors having components representing aircraft rotation about the predetermined axis and the locatio...