Inventive INS
How is range calculated by a DME?
Measuring the time interval between the interrogation and the response converted to range
Where are the rack hot sensors located
In the Computer/aviaonics rack next to the SPCU
What is Bernoulli's Principal and equation
An increase of dynamic pressure will bring about a decrease in static pressure
Pressure total = pressure static + pressure dynamic
DC and AC Power sources
BETS
Batteries x2 24 volt
External DC 28 volt
TRU x2 115AC to 28 DC
Starter/generator 28 Volt
GEIA
Generators x2 115volt
External 115
Inverters 28-115
APU 115
Schuler Period
84.4 Minutes
Where does the NTS Emulated INS receive its navigation and position information?
Sourced from the IRU
WX vs CTR Radar
WX = weather mode
CTR = Suppresses areas of high precipitation
What are the forces acting on an aircraft
1. Lift
2. Weight
3. Thrust
4. Drag
Max ramp, take off, and landing weight s
Ramp 34700
Take off 34500
Landing 33900
Information passed from the aircraft GPS to Emulated GPS
GPS Position
Time
Satilitte Info
System Status
Alititude
G/S
Ground Track
The NTS uses which geographic Datum at 402
Wgs-84
How/where/when is absolute altitude available on the GONZO
below 2500 ft AGL
Components of an Aircraft
Fuselage, Wings, Empennage
Fuel Capacity of Main and Aux Tanks
Main 5678
Aux 4566
What does a flashing and steady light mean for the King KHF 950 Radio
Flashing = tuning
Steady = Transmitting
Combining INS with any other Nav Sensor is Called?
Hybridization
1. Range
2. Azimuth
3. Elevation
4. Speed
Newton's Three Laws
1. Law of inertia (Motion =Motion)
2. Law of Acceleration (F=MA)
3. Law of action and reaction
Time of usable O2 For Crew
1800 psi 60/10
1300 psi 41/7
What does the alert annunciator on emulated INS mean
90 seconds from waypoint (or 90 to an abeam position if off track
Components of generic INS
Accelerometers
Computers
Stable Platform
Control and display unit
Components of the GONZO Radar (10)
1. Antenna
2. Waveguide Pressurization system
3. Power Supply
4. Receiver/Transmitter
5. Remote Radar Interface Unit (RRIU)
6. Navigation Training System Computer (NTSC)
7. SPCU
8. Pilot Control Panel
9. 20.1 LCD
10. ATS Controls
Axis of movement, control structure, and movement
Lateral -> Elevator -> Pitch
Vertical -> Rudder -> Yaw
Longitudinal -> Alierons -> Roll
Time of usable O2 for Pilots
1800 140/25
1300 98/17
What are the DADC Outputs
TAS
Pressure Altitude
OAT
Maximum Operating Speed
Uncorrected Pressure Altitude