Raytheon Anschütz Pilotstar D, Руководство пользователя

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HSC
P
ilotstar
D
III
3060.DOC012
Edition:
March
13,
2009
1.
Sensor
failures
No.
Action
Effect
Operator
Note
Reaction
time
1
Failure
of
the
log
If
NMEA
speed
is
disturbed
LOG
FAIL
is
announced
optically
and
acoustically
.
Switch
over
the
log
to
manual
speed
input.
The
reaction
time
--
switching
over
to
manual
input
--
is
not
critical
as
long
as
the
sp
ee
d
is
to
be
m
ai
n-
Plus
Log
Low
Speed
For
speeds
below
3
knots,
alarm
m
essage
Low
Speed
is
an-
nounced
optically
and
acoustically
on
the
control
unit.
“RELA
Y
S
A
LARM”
output
active
(see
section
4.7).
sp
ee
d
is
to
be
m
ai
n-
tained.
2
Error
in
the
heading
ref
-
erence
A
heading
reference
failure
is
sensed
and
announced
optically
and
acoustically
on
the
control
unit
as
Gyro
Fail
.
The
last
valid
actual
heading
is
frozen
and
is
used
from
then
on
as
the
heading
reference.
The
set
heading
should
be
the
same
as
the
actual
heading
in
order
to
prevent
any
rudder
reaction.
It
is
no
longer
possible
to
set
a
heading
on
the
control
unit.
a)
Reduce
the
speed
to
values
<
20
knots.
Switch
over
to
the
m
agnetic
compass
or
to
the
second
gyrocompass,
if
one
is
available. Optimize
the
control
parameters
during
magnetic
compass
operation
if
stable
regulation
is
not
available.
b)
Switch
over
to
manual
control
and
use
a
second
heading
reference
that
is
not
subject
to
errors.
“RELA
Y
S
A
LARM”
output
active
(see
section
4.7).
If
it
is
necessary
to
make
a
m
aneuver
,i
t
is
necessary
to
switch
over
immedi
-
ately
to
m
anual
control.