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What is an inertial navigation system (INS)
heading reference system that uses dead reckoning method of navigation
Define Dead Reckoning
process of estimating present position from known info
gyroscope
mechanical device containing a spinning mass universally mounted
The INS keeps track of and NOT __
position, total distance traveled
What kind of info does the INS provide?
Position
Inertial Navigation Unit: Platform Assembly
Sensors detect aircraft acceleration and altitude
Inertial Navigation Unit: Digital Computer
integration of platform signals
Air Data Computer
Provides barometric altitude, true airspeed, & magnetic heading to the INU
Digital Data Computer
performs interfacing between INS and other subsystems
EEC
Provides present position, elevation, and magnetic variation
Compass Controller
Provides switching functions, latitude compensation signals, and slew signals to the system compass adapter
Glide path
Predetermined imaginary path to the landing strip in the horizontal plane
Glide Slope
Predetermined imaginary path to the landing strip in the vertical plane
GPS is accurate in what dimensions?
Latitude
Longitude
Altitude
Identification Friend or Foe
Allows friendly craft to identify itself
reports altitude info to ground air control RADAR
operates up to 300 miles
Coder synchronizer unit
Synchronized to the radar system transmitter.
-fires 1 to 40 microseconds after the radar transmitter pulse
Transponder unit
-transmits reply pulses to the interrogator
-usually resides in aircraft
degress of freedom
Number of axis rotor is free to process
Define velocity
result of acceleration when intergraded with time
What is mechanical drift?
Slow procession caused by random inaccuracies
What is rate gyroscopes?
Restrained gyroscope with one degree of freedom
What is floated gyroscope?
Unit uses a restrained called a torsion bar
Accelerometer
Device that measures acceleration and develops proportional signal.
What are the types of accelerometers
Basic, E-Transformer, pulse continuing.
What is rigidty?
Ability of a gyroscope to keep axis fixed in space.
What is precession?
Rotation of spin axis of a gyroscope in response to attempt to move spin axis. Direction is always perpendicular.
What are the 3 directions an accelerometer is pointed?
North, East and vertical.
Define ground alignment mode
Mode of operation establishes the referenced which the INS determines aircraft altitude and measures acceleration to computer aircraft position.
Altitude heading references system (AHRS)
Supplies the flight instruments for pilot referencing with inputs representing Pitch, roll and yaw.
Displacement gyroscope
Hermetically sealed, two gyroscope platform providing pitch, roll and azimuth signals to the systems indication instruments.
Compass transmitter flux value
Senses the directions of the earths magnetic field and develops a proportional signal.
Compass mode (Comp)
Emergency mode used when the displacement gyroscope malfunctions.
Free mode (free)
Used at latitudes greater than 70 degrees.
Slaved mode (Salve)
Normal operation mode that uses both flux value and directional gyroscope signals
Angle of attack (AOA)
Angle between the chord line of an airfolc and the relative land
Automatic carrier landing system (ACLS)
Aids pilot in safely landing aircraft about an aircraft carrier. Does NOT guarantee perfect landing.
Data link
Pitch and roll commands that are used to intercept and lock onto landing pattern, data link commands that establish proper glide path
Landing control central system (LCCS)
Radar tracks aircraft and compass position to desired glide path
LCCS Mode 1
Fully automatic from entry point to touchdown
LCCS mode 2
Manual control of aircraft by pilot using cockpit displays
LCCS mode 3
Manual pilot control with talk down guidance by shipboard controller
ACLS Mode 1
Landing operation, pilot switches to ACL and verbally acknowledges engagement of autopilot.
Safety Provisions during ACLS mode 1
Global Positioning System
GPS System provides:
Passive operation, all-weather operations, real time position, continuous operation, usability in hostile environments, infinite number of users.
Aviation GPS
Vital for streaming en route, terminal and approach navigation. Reducing flight and saving fuel and money
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.
Identification: Friendly or foe
Interrogator unit
Pulse type transmitter that is triggered by coder synchronizer
Coder Synchronizer unit
Synchronized to the radar system transmitter. Fires 1 to 400 milliseconds after Rader transmitter pulse.
Transponder unit
Transmits reply pulses to the interrogator
Search radar unit
Initiates trigger pulse and radar video for unidentified craft.
IFF mode 1
Used for general ID of military aircraft only
IFF mode 2
Used for personal ID
IFF mode 3
Used in conjunction with ATC
IFF mode 4
Classified secure mode of operation
IFF mode C
Provides altitude INFO
IFF mode 4 computer
Allows IFF transponder to respond to secure mode 4 interrogations.
How long are interrogation pulses
0.8 - 11 Usec
What is the framing for information pulses?
45 Usec wide and 1.45Usec Apart
What is I/P (Identification of position)
Switch on EEC is pressed. Lasts for 15-30 seconds in mode 1 2 and 3A
What is emergency operation
What provides false reading or dangerous potentials even if power is off?
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