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82 Terms

1
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What is an inertial navigation system (INS)

heading reference system that uses dead reckoning method of navigation

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Define Dead Reckoning

process of estimating present position from known info

3
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gyroscope

mechanical device containing a spinning mass universally mounted

4
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The INS keeps track of and NOT __

position, total distance traveled

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What kind of info does the INS provide?

Position

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Inertial Navigation Unit: Platform Assembly

Sensors detect aircraft acceleration and altitude

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Inertial Navigation Unit: Digital Computer

integration of platform signals

8
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Air Data Computer

Provides barometric altitude, true airspeed, & magnetic heading to the INU

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Digital Data Computer

performs interfacing between INS and other subsystems

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EEC

Provides present position, elevation, and magnetic variation

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Compass Controller

Provides switching functions, latitude compensation signals, and slew signals to the system compass adapter

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Glide path

Predetermined imaginary path to the landing strip in the horizontal plane

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Glide Slope

Predetermined imaginary path to the landing strip in the vertical plane

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GPS is accurate in what dimensions?

Latitude

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Longitude

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Altitude

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Identification Friend or Foe

Allows friendly craft to identify itself

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reports altitude info to ground air control RADAR

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operates up to 300 miles

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Coder synchronizer unit

Synchronized to the radar system transmitter.

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-fires 1 to 40 microseconds after the radar transmitter pulse

22
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Transponder unit

-transmits reply pulses to the interrogator

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-usually resides in aircraft

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degress of freedom

Number of axis rotor is free to process

25
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Define velocity

result of acceleration when intergraded with time

26
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What is mechanical drift?

Slow procession caused by random inaccuracies

27
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What is rate gyroscopes?

Restrained gyroscope with one degree of freedom

28
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What is floated gyroscope?

Unit uses a restrained called a torsion bar

29
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Accelerometer

Device that measures acceleration and develops proportional signal.

30
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What are the types of accelerometers

Basic, E-Transformer, pulse continuing.

31
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What is rigidty?

Ability of a gyroscope to keep axis fixed in space.

32
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What is precession?

Rotation of spin axis of a gyroscope in response to attempt to move spin axis. Direction is always perpendicular.

33
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What are the 3 directions an accelerometer is pointed?

North, East and vertical.

34
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Define ground alignment mode

Mode of operation establishes the referenced which the INS determines aircraft altitude and measures acceleration to computer aircraft position.

35
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Altitude heading references system (AHRS)

Supplies the flight instruments for pilot referencing with inputs representing Pitch, roll and yaw.

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Displacement gyroscope

Hermetically sealed, two gyroscope platform providing pitch, roll and azimuth signals to the systems indication instruments.

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Compass transmitter flux value

Senses the directions of the earths magnetic field and develops a proportional signal.

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Compass mode (Comp)

Emergency mode used when the displacement gyroscope malfunctions.

39
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Free mode (free)

Used at latitudes greater than 70 degrees.

40
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Slaved mode (Salve)

Normal operation mode that uses both flux value and directional gyroscope signals

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Angle of attack (AOA)

Angle between the chord line of an airfolc and the relative land

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Automatic carrier landing system (ACLS)

Aids pilot in safely landing aircraft about an aircraft carrier. Does NOT guarantee perfect landing.

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Data link

Pitch and roll commands that are used to intercept and lock onto landing pattern, data link commands that establish proper glide path

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Landing control central system (LCCS)

Radar tracks aircraft and compass position to desired glide path

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LCCS Mode 1

Fully automatic from entry point to touchdown

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LCCS mode 2

Manual control of aircraft by pilot using cockpit displays

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LCCS mode 3

Manual pilot control with talk down guidance by shipboard controller

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ACLS Mode 1

Landing operation, pilot switches to ACL and verbally acknowledges engagement of autopilot.

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Safety Provisions during ACLS mode 1

  • Couple signal transmission ceases
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  • Auto pilot disengages
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  • Pilot must revert to mode II or III
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Global Positioning System

  • Navigation within 10 meters in 3D
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  • Velocity withing .1 meters/sec
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  • Time within 100 nanoseconds
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  • GPS Satellites use automatic clock w accuracy to approx
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  • 1 second per 20 million years
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GPS System provides:

Passive operation, all-weather operations, real time position, continuous operation, usability in hostile environments, infinite number of users.

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Aviation GPS

Vital for streaming en route, terminal and approach navigation. Reducing flight and saving fuel and money

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GPS Signal and Data flow

2 RF signals called link 1 (l-1) and link 2 (L-2). Antenna controller separates, amplifies and converts signals.

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Identification: Friendly or foe

  • Permits friendly craft to ID itself automatically
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  • Reports altitude info to ground ATC radar
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  • Range is approx 300 miles
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Interrogator unit

Pulse type transmitter that is triggered by coder synchronizer

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Coder Synchronizer unit

Synchronized to the radar system transmitter. Fires 1 to 400 milliseconds after Rader transmitter pulse.

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Transponder unit

Transmits reply pulses to the interrogator

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Search radar unit

Initiates trigger pulse and radar video for unidentified craft.

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IFF mode 1

Used for general ID of military aircraft only

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IFF mode 2

Used for personal ID

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IFF mode 3

Used in conjunction with ATC

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IFF mode 4

Classified secure mode of operation

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IFF mode C

Provides altitude INFO

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IFF mode 4 computer

Allows IFF transponder to respond to secure mode 4 interrogations.

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How long are interrogation pulses

0.8 - 11 Usec

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What is the framing for information pulses?

45 Usec wide and 1.45Usec Apart

75
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What is I/P (Identification of position)

Switch on EEC is pressed. Lasts for 15-30 seconds in mode 1 2 and 3A

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What is emergency operation

  • IFF master switch is set to EMERG
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  • Enabled when pilot Ejects
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  • Modes 1,2 and 3A are enabled to reply
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  • Mode 3A code becomes 7700
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  • Mode 4 operation is not affected by EMERG
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  • Overrides Emcon
82
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What provides false reading or dangerous potentials even if power is off?

AN/ARN 151 LAN