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An air data inertial reference unit (ADIRU) is a key component of the integrated air data inertial reference system (ADIRS), which supplies air data (airspeed, angle of attack and altitude) and inertial reference (position and attitude) information to the pilots' electronic flight instrument system displays as well as other systems on the aircraft such as the engines, autopilot, aircraft flight control system and landing gear systems.〔 〕 An ADIRU acts as a single, fault tolerant source of navigational data for both pilots of an aircraft.〔 〕 It may be complemented by a secondary attitude air data reference unit (SAARU), as in the Boeing 777 design.〔 (【引用サイトリンク】url=http://findarticles.com/p/articles/mi_m0UBT/is_12_21/ai_n27178496/?tag=content;col1 )〕 This device is used on various military aircraft as well as civilian airliners starting with the Airbus A320〔 〕 and Boeing 777. ==Description== An ADIRS consists of up to three fault tolerant ADIRUs located in the aircraft electronic rack, an associated control and display unit (CDU) in the cockpit and remotely mounted air data modules (ADMs).〔 〕 The No 3 ADIRU is a redundant unit that may be selected to supply data to either the commander's or the co-pilot's displays in the event of a partial or complete failure of either the No 1 or No 2 ADIRU. There is no cross-channel redundancy between the Nos 1 and 2 ADIRUs, as No 3 ADIRU is the only alternate source of air and inertial reference data. An inertial reference (IR) fault in ADIRU No 1 or 2 will cause a loss of attitude and navigation information on their associated primary flight display (PFD) and navigation display (ND) screens. An air data reference (ADR) fault will cause the loss of airspeed and altitude information on the affected display. In either case the information can only be restored by selecting the No 3 ADIRU.〔 Each ADIRU comprises an ADR and an inertial reference (IR) component. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「air data inertial reference unit」の詳細全文を読む スポンサード リンク
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