Can someone explain what is triple mix and how is it done? I know it is used in conjunction with INS systems to discover and minimize error but have not been able to find an explanation of it.
Many thanks!
Many thanks!
With all due respect, INS is still very much around, typically either GPS aided or GPS denied. That being said, I have no idea what “triple mix” is. Could he mean triplex?INS went away 20+ years ago.
With all due respect, INS is still very much around, typically either GPS aided or GPS denied. That being said, I have no idea what “triple mix” is. Could he mean triplex?
Nauga,
pedaling his Schuler cycle
INS went away 20+ years ago.
I got it Doc....
Really? In what?
There's definitely some terminology differences here. There are some aspects of commercial aviation (maybe not 121, I wouldn't know) that are still leveraging inertial nav to be functional in the absence of GPS. What you refer to as the IRS I have always understood to be the IRU, intertial reference unit(s), or IMU, inertial measurement unit(s); that an inertial nav system (INS) uses to estimate a position and nav solution. KVH and iMAR are two examples of current COTS INS producers, each with their own IMU. The days of iron gyros may be long gone, but LRGs and FOGs are still used.The old INS that were gyro backed are long gone from commercial aviation. Airliners and business jets today are using "IRS" (inertial reference system) that uses ring laser gyros and accelerometers to calculate positions. The IRS can be backed up with DME/VOR and GPS to enhance the position.
I have some experience with Kalman filters/LQE in nav and other applications and have never heard any part referred to as 'triple mix' - maybe it's application-specifc or deeper in the weeds of the sensor fusion than I typically go or something."Triple Mix" refers to the logic in the Kalman filters used to derive a single position solution.
There's definitely some terminology differences here. There are some aspects of commercial aviation (maybe not 121, I wouldn't know) that are still leveraging inertial nav to be functional in the absence of GPS. What you refer to as the IRS I have always understood to be the IRU, intertial reference unit(s), or IMU, inertial measurement unit(s); that an inertial nav system (INS) uses to estimate a position and nav solution. KVH and iMAR are two examples of current COTS INS producers, each with their own IMU. The days of iron gyros may be long gone, but LRGs and FOGs are still used.
I have some experience with Kalman filters/LQE in nav and other applications and have never heard any part referred to as 'triple mix' - maybe it's application-specifc or deeper in the weeds of the sensor fusion than I typically go or something.
Nauga,
tripley-mixed up
I'm thinking about Long Island Iced Teas.
Pretty much any airplane or weapon that has GPS-denied or GPS-unavailable capability. Most Navy airplanes (ASN-139), several civil/commercial airplanes (not 121) in development off the top of my head, I'm certain there are more.What aircraft still use INS?
Pretty much any airplane or weapon that has GPS-denied or GPS-unavailable capability. Most Navy airplanes (ASN-139), several civil/commercial airplanes (not 121) in development off the top of my head, I'm certain there are more.
Nauga,
and his niche market
Can someone explain what is triple mix and how is it done? I know it is used in conjunction with INS systems to discover and minimize error but have not been able to find an explanation of it.
Now that we got the dick length comparison out of the way:
How does the system decide if one of the sensors is too far off to contribute to a nav solution ?
https://www.amazon.com/dp/1420053086/How does the system decide if one of the sensors is too far off to contribute to a nav solution ?
If you consider condescending sniping about acronyms as part of that, sure then it was interesting.That was uncalled for. So far we've had an interesting discussion.
Pretty much any airplane or weapon that has GPS-denied or GPS-unavailable capability. Most Navy airplanes (ASN-139), several civil/commercial airplanes (not 121) in development off the top of my head, I'm certain there are more.
Nauga,
and his niche market
Now that we got the dick length comparison out of the way:
How does the system decide if one of the sensors is too far off to contribute to a nav solution ?
Now that we got the dick length comparison out of the way:
How does the system decide if one of the sensors is too far off to contribute to a nav solution ?
This is an old INS unit that was common place years ago.
Thanks for the positive contributions!
The question is based upon the DC0-10. My last job at UAL was maintaining the aircrew training material for that fleet. Way back in those pre GPS days the Diesel 10 used 3 INSs for overwater navigation and conventional VOR/DME fore domestic nav. Unfortunately the day overwater nav was covered in ground school I was out sick and was never able to attend a subsequent class. The concept has always been intriguing so thought it might spark a fun thread which it has.
My first job at UAL was teaching systems for the B-757/767. There was no GPS (1991ish) at that time so long range nav used three laser ring gyros. The Flight Management System used the information from traditional VOR/DME and the inertials to derive and update itself (if memory is correct it used DME/DME fixes then other fixes such as VOR crossing radials for updating...but that's going back several decades).
3-Why are their only 4,096 transponder codes?
Doc when I was involved with the 757/767 GPS was not in use by 121 carriers. Back then it was still under development and not installed in any UAL aircraft! After leaving that fleet circa 1993 and UAL circa 1996 I no longer had access to the FOM or the UAL training manual for that family. If you want to share this material I'd love to see it.
If not act like a professional and quit harping about my not looking it up!