| 摘要 |
<p>The method involves defining combinations of a set of control surfaces e.g. aileron, of an aircraft, and calculating an intermediate parameter (P) that is associated to an interaction coefficient (Pint) to form a pair of values (P1-P1, P2-P2, P3-P3, P4-P4) for each combination. A curve (C) is formed, where the curve defines the interaction coefficient according to the intermediate parameter from the pairs of values that are linked together by straight line segments (S1-S3). The curve is transmitted to a display unit. Independent claims are also included for the following: (1) a method for determining effectiveness of a combination of a set of control surfaces of an aircraft (2) an interpolation system (3) an assembly for determining overall effectiveness of control surfaces of an aircraft.</p> |
