A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 25_部分2.pdf400页

(c) AOA computation The A/C is wired in the AOA unique selection, so the ADR computes the AOA with the reading of one resolver. The second resolver is used as a back-up. The monitoring function is descibed in 34-18. The ADR determines the corrected angle of attack value which depends on the system number and the slat/flap position. For a CAS less than 60 kts: AOAc = 0 and status matrix is coded NCD. For a CAS more than or equal to 60 kts, the corrected angle of attack is calculated as follows: AOA ind AOAc = ------- + I K where: AOA ind = Indicated Angle of Attack (Ref. 34-11-00 for the relation between resolver and AOA indication) K, I = Correction coefficients which depend on system number, slat and flap configuration and magnitude AOA indication. The configuration is defined by the status of four input discretes (Ref. 2.A.(2)(c)). The results of the above computation is available on the labels: - label 221 = Indicated Angle of Attack - label 241 = Corrected Angle of Attack

R

EFF : CES

001-049, 101-105, 151-199, 201-203,

34-13-00 May 01/05 Page 13 Config-1


飞行翻译公司 www.aviation.cn
本文链接地址：A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 25_部分2.pdf