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时间:2010-05-30 09:34来源:蓝天飞行翻译 作者:admin
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I A R P Inver se Ad dress Resol u t ion Pro toc ol
IAS In dic a ted Ai r s peed is the speed indic a ted by a
di ffere n t ial press u re airspeed indic a tor th a t
mea s u res the actual press u re di ffere n t ial in the
pi to t - sta t ic hea d. It is the actual instrument
i n dic a t ion for a given fl ight con di t ion .
I ATA In tern a t ional Air Tra n s port Assoc ia t ion
I B AC In tern a t ional Bus i n ess Avia t ion Counc i l
I C ( 1 ) In tegra ted Circui t
( 2 ) In terc a bi n e t
I C AO In tern a t ional Civil Avia t ion Orga n iz a t ion (Mon trea l )
I C C IA PS Card Cage
I C C A I A In tern a t ional Coordi n a t i ng Council of Aeros pace
In dustries
I C D ( 1 ) In sta l la t ion Con trol Drawi ng
( 2 ) In terface Con trol Drawi ng
( 3 ) In teract ive Des ign Center
I C M In terline Com mun ic a t ions Ma nu a l
I C M P In ternet Con trol Message Pro toc ol
I C N I A In tegra ted Com mun ic a t ion s, Naviga t ion and
Id e n t i fic a t ion Avion ic s
I C P In i t ial Confl ict Pro be
I C S S In tegra ted Com mun ic a t ion Swi tch i ng Syste m
I C U In strument Com pa ra tor Un i t
I D Id e n t i fier
I D C In dic a tor Display / C on trol
I d e n t The act ion of the tra n s pon d er tra n s m i t t i ng an extra
p ul se along wi th its id e n t i fic a t ion code (at the request
of a con trol ler ).
I D I In i t ial Domain Id e n t i fier
H S AC E Horizon tal Sta bi l izer Act u a tor Con trol Electron ic s
H S- D S A D H igh Speed Fra me Re lay Service Access Device
H S I Horizon tal Situation In dic a tor. An indic a tor th a t
di s plays bea ri ng, g l id es lo pe, di sta nce, ra dio so u rce,
c o u r se and hea di ng inform a t ion .
H S I T Ha rdwa re and Softwa re In tegra t ion Test
H S L Hea di ng Se lect
H S R H igh Sta bi l i ty Refere nce
H S R P Hot Sta n dby Ro u t i ng Pro toc ol
H S TA Horizon tal Sta bi l izer Trim Act u a tor
H TC H ig h est Two - way Channel
H U D Head-Up Display
H V P S H ig h -Vol tage Power Supply
H W Ha rdwa re
H W C I Ha rdwa re Configu ra t ion Ite m
H X Heat Exch a nger
H Y D Hydraul ic
H Y D I M Hydraul ic In terface Module
H z Hertz (cyc les per sec on d )
I2S In tegra ted Inform a t ion Syste m
I AC S P In tern a t ional Aeron au t ical Com mun ic a t ions
Service Provid er
I / F In terface
I A 5 In tern a t ional A l p h a bet Num ber 5
I AG S In tegra ted A R INC Gro und Sta t ion
I A N A In ternet Ass ign ed Num ber Au th ori ty
I AOA In dic a ted Ang le - of - At tack
I AO PA In tern a t ional Council of Ai rc raft Own ers and
P i lo ts Assoc ia t ion s
4 8
5 1
I M C In strument Me teorological Con di t ion s
I M G Im ple me n ta t ionMa n age ment Gro u p
I M I Im bed d ed Message Id e n t i fier
I M O K I’m Ok ay
I M PAT T Im pact Ava la nche and Transmit Ti me.This type of
D i o d e diod e, when moun ted in an appro pria te cavi ty,
produces mic rowave osc i l la t ions and ampl i fic a t ion .
I n Inch
I N B D ( 1 ) Inboa rd
( 2 ) Inbo un d
I N D In dic a tor
I n d i c a t e d The altitude above mean sea level (unc orrected
A l t i t u d e for te m pera t u re ).
I N F O Inform a t ion Fra me
i n . h g. Inch es of Mercu ry
I N I T In i t ia l iz a t ion
I N J In ject ion
I N M A R S AT In tern a t ional Ma ri t i me Sa te l l i te Orga n iz a t ion
I N P H In terp h on e
I N S In ert ial Naviga t ion Syste m . A se l f - c on ta i n ed,
d ea d - reckon i ng system that se n ses the acce lera t ion
a long the th ree axes of the airc raft and calcula tes th e
di sta nce trave led from a refere nce poi n t . Accu racy
of the system dec rea ses wi th res pect to time.
I N S T In strume n t
I N TC In terce p t
I n t e r N I C In ternet Ne twork Inform a t ion Center
I n t r u d e r An altitude re port i ng airc raft that is be i ng con s id ered
as a po te n t ial th reat and processed by the th rea t
d e tect ion logic (TCA S ).
I / O Inp u t / O u tp u t . Refers to bi - di rect ional data ports.
I D G In tegra ted Drive Ge n era tor
I D P In i t ial Domain Pa rt
I D R P In ter- Domain Ro u t i ng Pro toc ol
I D S ( 1 ) Ice De tect ion Syste m
( 2 ) In tegra ted Display Syste m
( 3 ) Inform a t ion Display Syste m
I D U In teract ive Display Un i t
I E C IA PS Envi ronme n tal Con trol Module
I E D In sert ion Extract ion Device
I E E E In st i t u te of Electrical and Electron ic Engi n eer s
I E P R In tegra ted Engine Press u re Ratio
IF (if) In termedia te Freque nc y. A freque ncy to wh ich a
 
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