Moog Crossbow GNAV540 - Manual (Page 112)

GNAV540 User Manual
7430‐0808‐01 Rev. B
Page 112
Surfaced Submerged
UseMags ON 2 ON 3
UseGPS ON OFF
FreeIntegrate OFF OFF
Stationary Yaw Lock OFF OFF
Restart Over Range OFF OFF
Dynamic Motion ON ON
Turn Switch Threshold 10 deg/s 5 deg/s
Example
Table 98 below shows a typical flight profile of the fixed wing aircraft and the corresponding advanced settings that
can be configured per flight phase.
Table 98 Flight Profile Phases
Phase Description
Prelaunch The phase of flight in which an aircraft goes through a series of checkups (hardware and
software) on the ground before takeoff. The aircraft is a static condition,
Takeoff The phase of flight in which an aircraft goes through a transition from moving along the
ground (taxiing) to flying in the air, usually along a runway. The aircraft is under
nd horizontal acceleration and may suffer from vibrations coming from an engine and grou
contact forces transmitted from its landing gear..
Climb The phase of a flight, after takeoff, consisting of getting the aircraft to the desired flight
level altitude. More generally, the term 'climb' means increasing the altitude. The aircraft is
under vertical acceleration until it reaches the steady‐state climb rate.
Straight and level
flight
The phase of flight in which an aircraft reaches its nominal flight altitude and maintains it
speed and altitude. The aircraft is under equilibrium.
s
Maneuver The phase of flight in which an aircraft accelerates, decelerates, and turns. The aircraft is
under non‐gravitational acceleration and/or deceleration.
Descent The phase of flight in which an aircraft decreases altitude for an a
aircraft is under vertical deceleration until it captures a glide slop
pproach to landing. The
e.
Landing The last part of a flight, where the aircraft returns to the ground.
2 When not in distorted magnetic environment.