|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||706/023; 244/076R; 244/099.9; 701/003; 703/008|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 10|
A method for modeling error-driven adaptive control of an aircraft. Normal aircraft plant dynamics is modeled, using an original plant description in which a controller responds to a tracking error e(k) to drive the component to a normal reference value according to an asymptote curve. Where the system senses that (1) at least one aircraft plant component is experiencing an excursion and (2) the return of this component value toward its reference value is not proceeding according to the expected controller characteristics, neural network (NN) modeling of...
1. A method for modeling error-driven adaptive control of an aircraft, the method comprising: providing a selected aircraft variable, y(k+1), at a time index having a value k+1, as a matrix sum of Wf βf(k) and B u(k), where βf(k) includes the at least one aircraft variable y(k) in a linear or nonlinear format, Wf is a matrix of selected aircraft variable weighting coefficients, u(k) is a control variable vector for the at least one aircraft variable, and B is a matrix of control variable weighting coefficients that is not yet known;modeling an aircraft p...