| 摘要 |
<p>The method involves generating a roll objective, and determining effective values of parameters e.g. speed, of an aircraft. A deflection order is calculated on the basis of the roll objective and effective values. The deflection order is applied exclusively to airfoils of the aircraft, which are efficient on a roll axis to control the roll. A value is calculated on the basis of the roll objective. The deflection order is calculated on the basis of the value and effective values which comprise the effective value of the roll rate by using integration function. An independent claim is also included for an aircraft comprising a device for active controlling of a roll of the aircraft.</p> |
