SYSTEM AND METHOD FOR LIMITING CYCLIC CONTROL INPUTS
摘要
A control system having a first loop configured to provide a longitudinal blowback value of a rotor blade during flight and a second loop associated with the first loop, the second loop being configured to provide a design maximum total flapping value and a lateral flapping value. A method includes calculating a flight control limit from the design maximum total flapping value and the lateral flapping value. An upper longitudinal cyclic control limit is calculated by adding the flight control limit to the longitudinal blowback value. A lower longitudinal cyclic control limit is calculated by subtracting the flight control limit from the longitudinal blowback value.
申请公布号
CA2783118(C)
申请公布日期
2016.10.11
申请号
CA20122783118
申请日期
2012.07.11
申请人
BELL HELICOPTER TEXTRON INC.
发明人
FORTENBAUGH, ROBERT L.;RODRIGUEZ, JOSE MANUEL;KISOR, RONALD LORENZ;BLYTH, ROBERT