Auto-Coupled WAAS/DGPS Curved Approaches
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Auto-Coupled WAAS/DGPS Curved Approaches
Any reference material available regarding auto-coupled WAAS/DGPS curved approaches or auto-flight trajectories?
Thanx.
Thanx.
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Better to think of WAAS and DGPS as nav sensors rather than approach procedures.
FAA's LPV minima for RNAV (GPS) approaches require WAAS. However, LPV procedures have no curved paths.
You may be thinking of RNP SAAAR (ICAO = AR) procedures with RF (Radius to Fix) leg types.
Examples:
Queenstown
Chicago Midway
Rifle, CO
FAA AC 90-101 has more information
FAA's LPV minima for RNAV (GPS) approaches require WAAS. However, LPV procedures have no curved paths.
You may be thinking of RNP SAAAR (ICAO = AR) procedures with RF (Radius to Fix) leg types.
Examples:
Queenstown
Chicago Midway
Rifle, CO
FAA AC 90-101 has more information
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Dont think so. That is the whole point after all, to get away from the disadvantages of ground based aids.
The approaches I'm familiar with are designed without reference ground based aids.
The approaches I'm familiar with are designed without reference ground based aids.
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In my experience, crews are not permitted to "build" approaches, they must be in the database from an approved supplier, and arent to be modified.
Sure, you can build an approach using whatever waypoints you like but during a GPS or RNP approach you are asking the aircraft to fly a track determined in space by GPS.
In fact, some approaches ask you to deselect nearby navaids to prevent the chance of any radio updating so you dont inadvertantly get EPE exceeding the limit for the approach.
Sure, you can build an approach using whatever waypoints you like but during a GPS or RNP approach you are asking the aircraft to fly a track determined in space by GPS.
In fact, some approaches ask you to deselect nearby navaids to prevent the chance of any radio updating so you dont inadvertantly get EPE exceeding the limit for the approach.
In the case of DME and IRS, will the FMC generate some usable combined output during an RF leg?
It is the FMC that "projects or draws" the RF leg for the aircraft to fly. All the DME/DME or GPS does to the FMC position is increase accuracy and thefore the confidence of the FMC solution being where it was designed to be (RNP) this confidence is expressed as ANP (in nautical miles) on the Boeings. If you lose DME/DME or GPS updating the ANP (confidence of the FMC solution) will grow at the IRS drift rate until ANP is greater than the RNP. The IRS/FMC position may actually be bang on, but the confidence of the position gets worse over time.
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Can auto-coupled approach procedures involving Radius-to-Fix turns be performed with non-GPS nav-aids or some combination?
In the case of DME and IRS, will the FMC generate some usable combined output during an RF leg?
The ability of an FMS to fly various ARINC leg-types -- e.g., TF, RF, VA, CF, etc. -- is entirely separate from the position computation function.
Either the FMS can fly an RF leg or it cannot.
The sensors used to compute aircraft position are not relevant.
Having said that, I'm not aware of an FMS that is RF-capable that does not also have GPS sensors in the navigation array.
Having said that, I'm not aware of an FMS that is RF-capable that does not also have GPS sensors in the navigation array.
It is the GPS sensor equipment that provides a small enough ANP to fly an AR procedure with RF legs.
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Thanx for the info.
Is autopilot relied upon for legs with the lowest RNP values?
For an RNP leg of .1 for example, what ANP values are generally acheived by big Boeing and Airbus planes?
Is autopilot relied upon for legs with the lowest RNP values?
For an RNP leg of .1 for example, what ANP values are generally acheived by big Boeing and Airbus planes?
Last edited by Badmachine; 20th Jan 2009 at 05:38.