TAT total air temperature, is obtained by adding the heat due to friction of traveling at speed to your air temperature. For example, the temperature probe sticks out into 25 F air, but the airspeed is 225 kts., it will add a few degrees due to friction which is enough to throw off true airspeed calculations.
INS inertial navigation system, uses 3 actual rotating mechanical gyros to determine position, one each for pitch, roll and yaw, and definitely needs to be corrected from time to time when actual lat-long are known. Transoceanic aircraft originally used them before gps to get nav data on the open seas, away from radio navaids, but gps is taking its place since it is far more accurate and simple. Aircraft crossed the oceans and in the last 100 miles or so got a reference location from ATC before navigating to local destinations. Concorde and the MD11 used it, to name a few.
IRS inertial reference system, uses 3 ring lasers but does not require reference to known locations or calibration other than the initial fix. It uses the difference in the time it takes light to make its way around a triangular "ring" which indicates which path was shorter due to aircraft movement. Talk about sensitivity... plus they now are made the same size as a dime. I cannot name an aircraft that uses it, but there must be plenty. Rickair or one of the other aerospace people will have something hopefully to add.
I took a course at aerospace school called aircraft stability and spaceflight dynamics. They covered gyros among other things. It was an intense course, very good for understanding the math behind aircraft and satellite movements.
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Turn the heat O-F-F!
Last edited by Cubdriver : 05-15-2007 at 02:11 AM.
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