PHI - Position and Homing Indicator: Difference between revisions

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[[File:FIAT G91R1B gauge PHI - Position and Homing Indicator.jpg|thumb|PHI - Position and Homing Indicator]]
[[File:FIAT G91R1B gauge PHI - Position and Homing Indicator.jpg|thumb|PHI - Position and Homing Indicator]]
When you look at the cockpit of the [[http://wiki.flightgear.org/FIAT_G91R1B FIAT G91]] (but also of the F104) you can see in the center at the top a very particular instrument, particularly large and with 4 knobs on the sides. That instrument was one of the first navigation systems that used Doppler radar to determine ground speed.<BR>The accuracy of the instrument was, for those times, rather high, as it allowed to travel a long route up to 999 miles with a deviation in the position of the aircraft of 2-3%, a contained error that could be exploited both for flights both military and civilian in the transatlantic route, and in tactical flight in enemy territory or in areas with little radio assistance coverage. However, the real disadvantage in military use was that the instrument allowed to achieve this accuracy only with the use of the doppler radar, in the event that the pilot had disengaged the radar device, in order to be less visible to the enemy, the accuracy decreased a lot and was linked to the real knowledge of the local weather situation.
When you look at the cockpit of the [[FIAT G91R1B|FIAT G91]] (but also of the F104) you can see in the center at the top a very particular instrument, particularly large and with four knobs on the sides. That instrument was one of the first navigation systems that used Doppler radar to determine ground speed.
 
The accuracy of the instrument was, for those times, rather high, as it allowed to travel a long route up to 999 miles with a deviation in the position of the aircraft of 2-3%, a contained error that could be exploited both for flights both military and civilian in the transatlantic route, and in tactical flight in enemy territory or in areas with little radio assistance coverage. However, the real disadvantage in military use was that the instrument allowed to achieve this accuracy only with the use of the doppler radar, in the event that the pilot had disengaged the radar device, in order to be less visible to the enemy, the accuracy decreased a lot and was linked to the real knowledge of the local weather situation.


===Technique===
===Technique===
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[[File:PHI Station Selector - NCU in the FIAT G91R1B airplane.jpeg|thumb|PHI Station Selector - NCU in the FIAT G91R1B airplane]]
[[File:PHI Station Selector - NCU in the FIAT G91R1B airplane.jpeg|thumb|PHI Station Selector - NCU in the FIAT G91R1B airplane]]
Programming The instrument allows you to sequentially follow up to 5 routes stored in the '' Station Selector '' (unit with the code NCU located to the right of the pilot). A route consists of two values: N-S and E-W coordinates measured in air miles of the next point <ref name = "AD091920"/>. The NCU allowed the insertion of a box containing 4 multiturn resistors (10 turns) to enter the distance N-S and other 4 multiturn resistors to enter the distance E-W. Once the route was planned, the navigator made a list of max. 5 pairs of coordinates, the first pair was not inserted into the device, but only communicated to the pilot, who set it on the display, the other 4 pairs were set by a technician using a special programming device and a screwdriver that turned the potentiometers placed on the programming box. The cassette could be inserted into the compartment with a light pressure and extracted using the ''release'' button <ref name="release">The ''release'' button in the G91R1B works, and then ejects/retracts the program cassette.</ref> dell NCU unit.<br>Programming The instrument allows sequentially follow up to 5 routes stored in the ''Station Selector'' (unit with the code NCU located to the right of the pilot). A route consists of two values: N-S and E-W coordinates measured in air miles of the next point <ref name = "AD091920"/>.<br>In the simulation, as will see later, the two coordinates have been replaced by a distance and an angle (heading), with respect to the geographic North. In this way it is possible to quickly integrate the polar coordinate programming method of the routes obtained from the route manager of the FGFS program with the N-S and E-W system used by the PHI.
Programming The instrument allows you to sequentially follow up to five routes stored in the '' Station Selector '' (unit with the code NCU located to the right of the pilot). A route consists of two values: N-S and E-W coordinates measured in air miles of the next point <ref name = "AD091920"/>. The NCU allowed the insertion of a box containing four multiturn resistors (10 turns) to enter the distance N-S and other four multiturn resistors to enter the distance E-W. Once the route was planned, the navigator made a list of max. 5 pairs of coordinates, the first pair was not inserted into the device, but only communicated to the pilot, who set it on the display, the other four pairs were set by a technician using a special programming device and a screwdriver that turned the potentiometers placed on the programming box. The cassette could be inserted into the compartment with a light pressure and extracted using the ''release'' button <ref name="release">The ''release'' button in the G91R1B works, and then ejects/retracts the program cassette.</ref> dell NCU unit.
 
Programming The instrument allows sequentially follow up to 5 routes stored in the ''Station Selector'' (unit with the code NCU located to the right of the pilot). A route consists of two values: N-S and E-W coordinates measured in air miles of the next point <ref name = "AD091920"/>.
 
In the simulation, as will see later, the two coordinates have been replaced by a distance and an angle (heading), with respect to the geographic North. In this way it is possible to quickly integrate the polar coordinate programming method of the routes obtained from the route manager of the FGFS program with the N-S and E-W system used by the PHI.


===Parts constituting the apparatus===
===Parts constituting the apparatus===
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* Pitot tube to obtain the static and dynamic pressure without interfering with that used by the pneumatic instruments on board.
* Pitot tube to obtain the static and dynamic pressure without interfering with that used by the pneumatic instruments on board.
* Gyro Compass with fluxgate magnetic sensor.
* Gyro Compass with fluxgate magnetic sensor.
Inside the pilot's cabin:
Inside the pilot's cabin:
* Indicator Unit normally placed in front of the pilot at the top of the cockpit.
* Indicator Unit normally placed in front of the pilot at the top of the cockpit.
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Looking at the ''Route Manager'' ('''RM''') table, it can be seen that there is always an angle (ODO) with respect to the north and the length of the section to be covered. The last stretch is the one in sight of the airport and must be managed differently with the classic methods of instrumental or visual navigation.
Looking at the ''Route Manager'' ('''RM''') table, it can be seen that there is always an angle (ODO) with respect to the north and the length of the section to be covered. The last stretch is the one in sight of the airport and must be managed differently with the classic methods of instrumental or visual navigation.


To load the data into the PHI table (in fact it is as if you were programming the "Selector Unit Programmer" ('''NCU''') portable cassette, just click on the [Activate] button of the '''RM'''. you go now on the menu [''Fiat G91''] followed by [''PHI - route system''] opens a window showing various parameters among which we highlight 5 columns that correspond to the 5 'buttons '''NCU''', these columns have been filled in by the distance to cover, the direction and finally the altitude of the flight obtained by the Route Manager (if the altitude is zero in the '''RM''' this is set to 15,000 ft).
To load the data into the PHI table (in fact it is as if you were programming the "Selector Unit Programmer" ('''NCU''') portable cassette, just click on the [Activate] button of the '''RM'''. you go now on the menu [''Fiat G91''] followed by [''PHI - route system''] opens a window showing various parameters among which we highlight five columns that correspond to the five 'buttons '''NCU''', these columns have been filled in by the distance to cover, the direction and finally the altitude of the flight obtained by the Route Manager (if the altitude is zero in the '''RM''' this is set to 15,000 ft).


The PHI programming framework also contains other parameters among which we have the convergence <ref>The ''convergence'' is a necessary parameter for calculating rhumb line air routes and is calculated as the average of the latitude of the departure airport and of the arrival airport. The PHI allowed the programming of the convergence through a special panel, in case it was used in civil aviation or on military transport air vehicles, or through a regulator placed in the ``Signal amplifier and Junction-Box'' regulated by a specialized technician, in what required the opening of a special external door.</ref>
The PHI programming framework also contains other parameters among which we have the convergence <ref>The ''convergence'' is a necessary parameter for calculating rhumb line air routes and is calculated as the average of the latitude of the departure airport and of the arrival airport. The PHI allowed the programming of the convergence through a special panel, in case it was used in civil aviation or on military transport air vehicles, or through a regulator placed in the ``Signal amplifier and Junction-Box'' regulated by a specialized technician, in what required the opening of a special external door.</ref>
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* ''Route manager'': the data has been loaded from '''RM'''.
* ''Route manager'': the data has been loaded from '''RM'''.
[[File:Route programming table to be entered in the PHI memory.jpeg|thumb|Route programming table to be entered in the PHI memory]]
[[File:Route programming table to be entered in the PHI memory.jpeg|thumb|Route programming table to be entered in the PHI memory]]
In reality the 5 columns corresponded to the programming of only 4 columns, the first was set manually by the pilot.
In reality the five columns corresponded to the programming of only four columns, the first was set manually by the pilot.
 
The [Auto push] button allows to obtain the automatic progression of the route, in reality it was manual, obviously you can decide the progression manually.
 
The next block is the insertion of the magnetic declination, also in this case it is automatic, at least that the pilot does not want to do it himself.
 
The ''Wind configuration'' is used to automatically enter the wind direction and speed, otherwise it must be entered manually with the appropriate PHI system gauge.
 
Finally there is the section ''doppler''which defines four possible ways of use:
* OFF
* Rec only (keeping the doppler ''warm'', but without signal emission, useful in the enemy area)<ref>In reality, the ''heating'' time of the PHI apparatus was fairly long, it could proceed for several minutes before the thermionic valves stabilized, in the simulation this time was reduced to a few tens of seconds in order not to bore the user.</ref>
* ON (Operative)
* Test
 
The selector ''sea / land'' allows you to adjust a filter that improves the Doppler's operability when you have to cross a stretch of sea.


The [Auto push] button allows to obtain the automatic progression of the route, in reality it was manual, obviously you can decide the progression manually.<br> The next block is the insertion of the magnetic declination, also in this case it is automatic, at least that the pilot does not want to do it himself.<br>The ''Wind configuration'' is used to automatically enter the wind direction and speed, otherwise it must be entered manually with the appropriate PHI system gauge.<br>Finally there is the section ''doppler''which defines 4 possible ways of use:<br>OFF, Rec only (keeping the doppler ''warm'', but without signal emission, useful in the enemy area)<ref>In reality, the ''heating'' time of the PHI apparatus was fairly long, it could proceed for several minutes before the thermionic valves stabilized, in the simulation this time was reduced to a few tens of seconds in order not to bore the user.</ref>, ON (Operative), Test.<br>The selector ''sea / land'' allows you to adjust a filter that improves the Doppler's operability when you have to cross a stretch of sea.
{{Appendix}}

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