I've got pressure altitude and baro, is this correct?
Amsl = Ap + (baro - 29.92) x 1000
Example:
Pressure Altitude: 1141
Baro: 30.03
Amsl = 1141 + (30.03 - 29.92) * 1000 = 1251
I've got pressure altitude and baro, is this correct?
Amsl = Ap + (baro - 29.92) x 1000
Example:
Pressure Altitude: 1141
Baro: 30.03
Amsl = 1141 + (30.03 - 29.92) * 1000 = 1251
I like that.A quicker way, for me at least, to do this in my head, or with very minimal writing down, is converting the altimeter settings into "feet" by removing the decimal and adding a zero. i.e 29.92 becomes 29920. So 30.03 is 30030 - 29920 to get change in feet.
I would just write down the 30030 above the 29920 and subtract.
I remember the +/- by remembering that when I increase the altimeter setting, by turning the knob clockwise, the altitude increases.
We all think about these things differently, though, so that might work at all for you.
I don’t think my computer cares. And on that note, what would be the more accurate formula rather than the approximation?A quicker way, for me at least, to do this in my head, or with very minimal writing down, is converting the altimeter settings into "feet" by removing the decimal and adding a zero. i.e 29.92 becomes 29920. So 30.03 is 30030 - 29920 to get change in feet.
I would just write down the 30030 above the 29920 and subtract.
I remember the +/- by remembering that when I increase the altimeter setting, by turning the knob clockwise, the altitude increases.
We all think about these things differently, though, so that might work at all for you.
I have some telemetry that does not provide indicated altitude, but does provide pressure altitude and baro setting. This is not for in flight purposes.Why are we doing this calculating? I do it by setting baro in the box and reading the Altimeter. What am I missing here?
Pressure Altitude Correction = 145442.2*(1- (Baro/29.92126)^0.190261)I don’t think my computer cares. And on that note, what would be the more accurate formula rather than the approximation?
And it's not in contact with the ground in any way? Slant range and declination are not available?I have some telemetry that does not provide indicated altitude, but does provide pressure altitude and baro setting. This is not for in flight purposes.
Where is pressure altitude in that formula? I’m guessing 145442.2Pressure Altitude Correction = 145442.2*(1- (Baro/29.92126)^0.190261)
You'll still have to account for whether you add or subtract. This comes out with a negative number. If you use a sperad sheed, just wrap it in the abs function to geta a positive number if that's what you prefer.
The readings are taken in flight. I’m doing the calculations after the flight not during.And it's not in contact with the ground in any way? Slant range and declination are not available?
I didn't see a reference to a computer (or calculator). I described my method for making such calculations in the cockpit.I don’t think my computer cares.
No worries, just explaining my use case.I didn't see a reference to a computer (or calculator). I described my method for making such calculations in the cockpit.
I'm not sure what you mean. All this is calculating is the correction based on non-standard baro, the full formula that the (baro - 29.92) x 1000 rule of thumb is based on. In your example, the rule of thumb gives you the 110' approximation; the full calculation gives you 100.418' In both cases, you need to add or subtract the result from the pressure altitude you say you already have.Where is pressure altitude in that formula? I’m guessing 145442.2
I needed this to understand what you posted:I'm not sure what you mean. All this is calculating is the correction based on non-standard baro, the full formula that the (baro - 29.92) x 1000 rule of thumb is based on. In your example, the rule of thumb gives you the 110' approximation; the full calculation gives you 100.418' In both cases, you need to add or subtract the result from the pressure altitude you say you already have.
The formula is from Ed Williams "Aviation Formulary." I don't pretend to understand it any more than I understand the "real" density altitude calculation using Kelvin (or 90% of the calculations Ed shows)
OK. Sorry. I just understood that if I am given P_Alt, the correction gets applied to it and if I have Ind_Alt, the correction gets applied to that, just like in the rule of thumb version, so I missed that you needed that.I needed this to understand what you posted:
P_alt= Ind_Alt + P_alt_corr
Ind_Alt = P_Alt ± P_alt_corr
yeah, the link you sent was perfect. Thanks.OK. Sorry. I just understood that if I am given P_Alt, the correction gets applied to it and if I have Ind_Alt, the correction gets applied to that, just like in the rule of thumb version, so I missed that you needed that.
Since you did, I guess I'll mention that in your case, whether the correction is positive or negative depends on whether Baro is higher or lower than standard and that the algebraic equation needs to be turned around to:
since you already know P_Alt.Code:Ind_Alt = P_Alt ± P_alt_corr