Raytheon Beech Baron E55 - Page 559

BARON
55
AND 58
SHOP
MANUAL
return
the
airplane
to
straight flight.
Turns
or
beam
fol-
pitch
control
system
does
not
use
a
gyro
for
reference,
lowing
is
made
by
rotating
a
valve
sleeve
wiht
a
torqu-
but
uses
the
airspeed,
rate-of-airspeed
change
and
ing
movement
proportional
to
the
voltage
imposed
inertial
signals
to
control
the elevator
through
the
pitch
upon
it.
This
unit also
supplies
an
output
voltage
pro-
servos.
An
altitude hold
sensing
unit works
in
conjunc-
portional
to
the
turning
rate
that
is used
for
dip
com-
tion with
the
pitch
control to
sustain
a
given
altitude.
pensation
and
the
nose-up
signal
during
turns.
The
515
11-79