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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/52 ; 244/76 ; R|
|발명자 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 1|
A system for stabilizing an aircraft includes sensors positioned and disposed at predetermined locations on the aircraft and structured for sensing external forces acting on the aircraft at the sensor locations as a result of rapid changes in atmospheric conditions such as those associated with air turbulence and wind shear. A computer processor receives data from the sensors and activates one or more thrust generators positioned at predetermined locations of the aircraft to counteract the external forces and maintain the desired attitude and stability o...
An aircraft stabilizing system for use on aircraft having a fuselage section and wings comprising: sensing means positioned and disposed at a plurality of predetermined locations on the aircraft for detecting and measuring external forces exerted on said aircraft due to sudden changes in atmospheric pressure at said predetermined locations, thrust means for providing a propulsive force sufficient to counteract said external forces detected by said sensing means so that said external forces and said propulsive force are in equilibrium, thereby maintaining...