Not a great circle.
Equal distance from the poles.
A plane parallel to the polar axis.
The only fixed reference point on the Earth.
Parallels of equator.
Parallels of latitude.
Meridians of equator.
Meridians of longitude.
Equator.
Polar axis.
Greenwich meridian.
International time line.
0° to 90°N.
0° to 90°S.
0° to 180°N.
0° to 180°S.
0° to 90°N.
0° to 90°S.
0° to 180°N.
0° to 180°S.
Circle designated 10 degrees latitude.
Meridian designated the 180 degrees meridian.
Meridian passing through Greenwich, England.
Circle equal distance between the north and south poles.
Circle designated 0 degrees latitude.
Meridian designated the 180 degrees meridian.
Meridian passing through Greenwich, England.
Circle equal distance between the north and south poles.
0° to 90° east.
0° to 90° west.
0° to 180° east.
0° to 180° west.
0° to 90° east.
0° to 90° west.
0° to 180° east.
0° to 180° west.
0°.
90°.
North.
Equator.
0°.
90°.
180°.
270°.
Zero degrees to the object.
The object to true north.
True north to the object.
The aircraft heading to the object.
50°.
270°.
310°.
320°.
250 NM
300 NM.
350 NM.
400 NM.
Slight.
Negligible.
Significant.
Unimportant.
45°/15 knots.
225°/15 knots.
225° to 45°/15 knots.
45° from 225°/15 knots.
Yaw.
Drift.
Deviation.
Groundspeed.
Drift.
Airspeed.
Velocity.
Groundspeed.
Increase in ground speed with right drift.
Decrease in ground speed with right drift.
Increase in ground speed with no change in track.
Decrease in ground speed with no change in track.
Drift correction.
Wind disbursement.
Airspeed correction.
Ground speed correction.
Flight path.
Wind triangle.
Navigation chart.
Destination chart.
North pole.
South pole.
Magnetic north.
Magnetic south.
Equator.
Zero degrees meridian.
Magnetic poles.
Geographical poles.
Agonic lines.
Isogonic lines.
Variation lines.
Deviation lines.
Agonic lines.
Isogonic lines.
Variation lines.
Deviation lines.
Wind.
Airspeed.
Wind resistance.
Aircraft acceleration.
Altitude.
Coordinate system.
Frame of reference.
Frame of displacement.
Platform.
Integrator.
Summing unit.
Accelerometer.
Computer.
Platform.
Integrator.
Accelerometer.
Motion and pressure changes.
Magnetic and motion changes.
Temperature and pressure changes.
Temperature and magnetic changes.
One.
Two.
Three.
Four.
Speed.
Motion.
Velocity.
Reference.
Speed.
Motion.
Velocity.
Reference.
Speed.
Motion.
Velocity.
Reference.
One.
Two.
Three.
Four.
Two ring laser gyros and two accelerometers.
Three ring laser gyros and three accelerometers.
Two ring laser gyros, two accelerometers, and two synchro repeaters.
Three ring laser gyros, three accelerometers, and three synchro repeaters.
Altitude.
System status.
Present position.
Grid mode heading.
Causes a stability circuit to generate a voltage.
Causes a single-axis sensor to generate voltage.
Causes a proximity detector to generate a voltage.
Causes a fringe pattern detector to generate a voltage.
Time.
Distance.
Drift angle.
True airspeed.
Self test.
Navigation.
Allignment.
Initialization.
Automatically restart.
Stop and await a manual restart.
Be prolonged by no more than period of suspension.
Be prolonged by no more than period of suspension plus 20 seconds.
Better than 1.0 nautical miles/hour.
Better than 1.5 nautical miles/hour.
Better than 2.0 nautical miles/hour.
Better than 2.5 nautical miles/hour.
At all times.
Only when manually selected.
Automatically upon failure of INS/GPS solution.
Automatically upon failure of GPS-only solution.
Pure inertial.
Precise positioning service.
Global positioning system (GPS) only.
Blended inertial navigation system (INS)/GPS.
6 hours.
12 hours.
24 hours.
48 hours.
None.
One.
Two.
Three.
Dividing the time by the range.
Adding the distance to four satellites.
Decoding the radio frequency signal transmitted.
Measuring the rate of change of the radio frequency signal.
EPE < 25 meters.
101 ≤ EPE < 200 meters.
201 ≤ EPE < 500 meters.
EPE > 5000 meters.
50.
100.
150.
200.
Antenna.
Receiver.
Indicator control.
Antenna controller.
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