Trio Avionics Pro Pilot - Chapter 1 Horizontal Navigation Overview (HNAV); GPS Requirements; Basic H NAV Operation Modes

Trio Pro
P
Ho
The H N
A
provides
GPS
R
The Pro
P
appropri
a
time of i
n
The Pro
P
GPS digi
format o
r
the GPS
S
Opera
t
While th
e
from a G
complex,
Three h
o
Basic
The cap
a
1.)
T
2.)
C
3.) I
4.)
W
N
p
e
t
o
E
i
n
P
ilot Manual
4
rizon
AV
function
o
horizontal n
a
R
equirem
e
P
ilot does no
t
a
te host GPS
n
stallation. (S
e
P
ilot uses a
s
tal data stre
a
r
the Aviation
S
and GPSV
t
ion
e
Pro Pilot is
a
PS source.
T
multi-segm
e
o
rizontal navi
g
H
NAV O
p
a
bilities of th
e
T
rack Mode t
r
C
ourse Mode
ntercept Mod
W
hen directe
d
ote: The Pro
e
rformance
a
o
thermal shif
t
EPROM me
m
n
formation du
4
.1
tal N
a
o
f the Pro Pil
o
a
vigation usin
g
e
nts
t
contain a b
u
source be s
u
e
e the Install
a
s
olid-state in
e
a
m for the na
v
Link format f
o
options.
a
n excellent
“
T
his can be a
s
e
nt flight plan.
g
ation modes
p
eration
M
e
H NAV syst
e
r
acks a GPS
d
tracks a pilo
t
e flies the ai
r
d
, execute a
1
Pilot also us
e
nd provides
a
t
s, inherent s
e
m
ory that is u
p
r
ing each flig
h
Ch
a
a
viga
t
o
t controls th
e
g
signals fro
m
u
ilt-in GPS or
u
pplied and c
o
a
tion Instruct
i
e
rtial rate sen
s
v
igation funct
i
o
r navigation
“
wing leveler,
”
s
simple as
a
allow the pil
o
M
odes
e
m comprise
d
irected fligh
t
t
directed he
a
r
plane back t
o
1
80 degree c
o
e
s the GPS
d
a
utomatic co
r
e
nsor drift an
p
dated auto
m
h
t.
a
pter
t
ion
O
e
roll axis ser
v
m
a GPS rec
e
other naviga
t
o
rrectly conn
e
ons later in t
h
s
or for attitud
i
on. It accep
t
guidance.
A
”
its greatest
s
a
“GOTO” a
w
o
t to follow a
s
four basic m
o
t
plan course
l
a
ding.
o
a previousl
y
o
urse revers
a
d
erived infor
m
r
rections to th
d noise error
s
m
atically with
t
1
O
ver
v
v
o for attitud
e
e
iver or EFIS
tion data sou
e
cted to the
C
h
is manual.)
e stabilizatio
n
t
s either a N
M
A
n ARINC 42
9
strength is fo
w
aypoint as c
o
s
elected GP
S
o
des:
l
ine.
y
entered cou
a
l
m
ation to mon
h
e sensor dat
a
s
. The Pro P
t
he most cur
r
v
iew (
e
correction (
w
system.
rce. It is nec
C
ontrol and
D
n
. It uses ele
M
EA 0183, V
2
9
upgrade is
a
llowing an a
c
o
mmanded b
y
S
course or fl
i
rseline.
itor the inerti
a
a
to correct f
o
P
ilot has a fla
s
r
ent dynamic
HNA
V
w
ing leveling)
essary that a
D
isplay Head
e
ments of the
2
.XX stream
a
vailable to e
n
c
tive flight pla
n
y
the GPS, o
r
i
ght plan.
a
l sensor
o
r drift due
s
h based
calibration
8
V
)
and
n
at the
host
nable
n
r
a