|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/434 ; 364/433 ; 318/584 ; 244/177|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 15|
A flight control system utilizing multi-controlled surfaces to provide the necessary control power and feedback logic to stabilize the aircraft with minimal noise amplification. In addition, a unique performance optimization loop is integrated into the stability logic to position the multi-control surfaces for optimum maneuver performance.
In a flight control system for an aircraft having three control surfaces, interconnected feedback control loops for stabilizing and optimizing the performance of the aircraft, the stabilizing loop comprising: first means for summing signals representing pitch rate and vertical acceleration of the aircraft; complementary filter means connected at its input to the pitch rate signal and a canard position signal for filtering these signals together to form a combined signal thereby reducing signal noise; second means for summing the combined signal and an ou...