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G S P G la re Shie ld Pa n e l
G S V G ray Sc a le Vol tage ( s )
GT G rea ter T h a n
GTA Ge n eral Terms Agree me n t
GTC Da ta Link Gro und Terminal Com p u ter
GT R Ge n eral Tech n ical Requi re me n ts
G U I G ra p h ic / User In terface
G V E G ra p h ics Vector Engi n e
G W Ga teway
G W S G ra p h ical Wea th er Services
G y r o s c o p e A ro ta t i ng device that will maintain its original pla n e
of ro ta t ion , no matter wh ich di rect ion the gyrosc o pe
m o unt is turn ed.
H A D Ha rdwa re Arch i tect u re Docume n t
H A M S Hot Air Ma n age ment Syste m
G N D G ro un d
G N E G ross Naviga t ional Error
G N R G lo bal Naviga t ion Rece iver
G N S S G lo bal Naviga t ion Sa te l l i te Syste m
G N S S P G lo bal Naviga t ion Sa te l l i te System Pa n e l
G o n i o m e t e r A d evice that com bi n es the two signals from two loo p
a n te n n a s.The gon iome ter (or resolver) con tains two
fi xed coils and one ro ta t i ng coi l .The ro ta t i ng coil is
c on n ected to the A DF bea ri ng indic a tor needle to
i n dic a te the re la t ive bea ri ng from the airc raft to th e
N DB sta t ion .The mech a n ical pos i t ion of the ro tor
re prese n ts the bea ri ng of the sta t ion , and the pos i t ion
is electric a l ly tra n s m i t ted to the RMI.
G O S G rade of Service
G O S I P Government Open Systems In terc on n ect ion Profi le
G PA D I R S G lo bal Pos i t ion i ng, Air Da ta , In ert ial Refere nce Syste m
G P I B Ge n eral Purpose In strument Bus
G P P Ge n eral Purpose Processor
G P S ( 1 ) G lo bal Pos i t ion i ng System (See NAVSTA R )
( 2 ) G lo bal Pos i t ion i ng Sa te l l i te
GPS L1 G lo bal Pos i t ion i ng System L1 Freque nc y
G P S S U G lo bal Pos i t ion i ng System Se n sor Un i t
G P U G ro und Power Un i t
G P W C G ro und Proxi m i ty Wa rn i ng Com p u ter
G P W S G ro und Proxi m i ty Wa rn i ng Syste m
G R G ro und Ro u ter
G R I B G rid d ed Bi n a ry (Na t ional Wea th er Service
Mod e l O u tp u t )
G r a d i e n t The ra te at wh ich a va ria ble qu a n t i ty inc rea ses
or dec rea ses.
4 4
4 7
H G C Head-Up Guid a nce Com p u ter
H G S Head-Up Guid a nce Syste m
H H L D Hea di ng Hold
H I H ig h
H I C Head Im pact Cri teria
H I L Horizon tal In tegri ty Limit
H I R F ( 1 ) H igh In te n s i ty Radia ted Fie ld
( 2 ) H igh In te n s i ty Radio Freque nc y
H L C S H igh Lift Con trol Syste m
H L E H ig h er Layer En t i ty
H L L H igh Level Langu age
H M I Human Machine In terface
H M O S H igh De n s i ty Me tal Oxide Se m ic on ductor
H M U He ight Mon i tori ng Un i t
H O Ha n d off
H O W Hand Over Word
H P ( 1 ) H igh Press u re
( 2 ) Holdi ng Pa t tern
H PA H igh Power Am pl i fier
h Pa h ecto Pa sc a l
H P C H igh Press u re Com pressor
H - P l a n e The H-Plane is the plane in wh ich the magn e t ic fie ld
of the antenna lies. The H-Plane is perpe n dicular to
the E- Pla n e.
H P R H ig h - Power Re lay
H P R E S P ress u re A l t i t u d e
H P S OV H ig h - P ress u re Shutoff Va lve
H P T H ig h - P ress u re Tu r bi n e
H R D Home Ro u t i ng Dom a i n
H S A Horizon tal Sta bi l izer Act u a tor
H A R S H igh Altitude Ro u te Syste m
HCP Head-Up Con trol Pa n e l
HCI Human Com p u ter In terface
H C S Host Com p u ter Syste m
H C W Heavi ly Cold Wor ked Pipe and Tu be (Sea n - Free ™ )
H D B K Ha n dboo k
H D G Hea di ng
HDG SEL Hea di ng Se lect
H D I S K Ha rd Disk
H D L Hy brid Da ta Link
H D L C H ig h - Level Da ta Link Con trol
H D L C- B H ig h - Level Da ta Link Con trol - Ba la nced
H D L M S Hy brid Da ta Link Ma n age ment Syste m
H D O P Horizon tal Dilution of Prec i s ion
H D OT In ert ial Vert ical Speed
H D P Ha rdwa re Deve lo pment Pla n
H E Altitude Error
H e a d i n g The di rect ion of an airc raft pa th wi th res pect to
m agn e t ic or true north .
H F H igh Freque nc y.The port ion of the ra dio spectrum
from 3 to 30 MHz. HF com mun ic a t ion syste m s
o pera te in the 2 to 30 MHz port ion of the spectrum .
H F D L H ig h - Freque ncy Da ta Link
H F D M HF Da ta Mod e m
H F D R H igh Freque ncy Da ta Radio
H F N P D U H igh Freque ncy Ne twork Pro toc ol Da ta Un i t
H F S H igh Freque ncy Syste m
H F S G Human Factor Study Gro u p
H F S N L HF SubNe twor kL ayer
H G A H igh Gain An te n n a
4 6
4 9
I A PA In strument A p proach Procedu res Au tom a t ion
I A P S In tegra ted Avion ics Process i ng Syste m
　
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