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1) Air_Temp_w: Air Temperature Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] | |||
2) MachNo_w: Mach Number based on Wing Pitot Pressure | |||
3) IAS_w: Indicated Air Speed based on Wing Pitot Pressure [m/s] | |||
4) TAS_w: True Air Speed based on Wing Pitot Pressure [m/s] {Calibration: slope = 60.797701 offset = -150.48263} | |||
5) Press_Alt: Pressure Altitude [m] | |||
6) Alpha_nose: Alpha (Attack) Angle based on Nose Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} | |||
7) Beta_nose: Beta (Sideslip) Angle based on Nose Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} | |||
8) GS_X: X (East) Component of the Ground Speed [m/s] | |||
9) GS_Y: Y (North) Component of the Ground Speed [m/s] | |||
10) VERT_VEL: Vertical Velocity of the aircraft based on the change in position over a 2 seceond interval [m/s] | 10) VERT_VEL: Vertical Velocity of the aircraft based on the change in position over a 2 seceond interval [m/s] | ||
11) Wind_X_Nose: X (East) Component of the Wind Speed based on the Nose Probe [m/s] | 11) Wind_X_Nose: X (East) Component of the Wind Speed based on the Nose Probe [m/s] | ||
12) Wind_Y_Nose: Y (North) Component of the Wind Speed based on the Nose Probe [m/s] | 12) Wind_Y_Nose: Y (North) Component of the Wind Speed based on the Nose Probe [m/s] | ||
13) Wind_Z_Nose: Z (Vertical) Component of the Wind Speed based on the Nose Probe (postive value is upward, away from the Earth's surface) [m/s] | 13) Wind_Z_Nose: Z (Vertical) Component of the Wind Speed based on the Nose Probe (postive value is upward, away from the Earth's surface) [m/s] | ||
14) Wind_M_Nose: Horizontal Wind Speed based on the Nose Probe [m/s] | 14) Wind_M_Nose: Horizontal Wind Speed based on the Nose Probe [m/s] | ||
15) Wind_D_Nose: Horizontal Wind Direction from Nose Probe [degrees]; True Direction From Which it Blows | 15) Wind_D_Nose: Horizontal Wind Direction from Nose Probe [degrees]; True Direction From Which it Blows | ||
16) Wind_X_Wing: X (East) Component of the Wind Speed based on the Wing Probe [m/s] | 16) Wind_X_Wing: X (East) Component of the Wind Speed based on the Wing Probe [m/s] | ||
17) Wind_Y_Wing: Y (North) Component of the Wind Speed based on the Wing Probe [m/s] | 17) Wind_Y_Wing: Y (North) Component of the Wind Speed based on the Wing Probe [m/s] | ||
18) Wind_Z_Wing: Z (Vertical) Component of the Wind Speed based on the Wing Probe (positive value is upward, away from the Earth's surface) [m/s] | 18) Wind_Z_Wing: Z (Vertical) Component of the Wind Speed based on the Wing Probe (positive value is upward, away from the Earth's surface) [m/s] | ||
19) Wind_M_Wing: Horizontal Wind Speed based on the Wing Probe [m/s] | 19) Wind_M_Wing: Horizontal Wind Speed based on the Wing Probe [m/s] | ||
20) Wind_D_Wing: Horizontal Wind Direction from Wing Probe [degrees]; True Direction From Which it Blows | 20) Wind_D_Wing: Horizontal Wind Direction from Wing Probe [degrees]; True Direction From Which it Blows | ||
21) Wind_X: X (East) Component of the Wind Speed [m/s] | 21) Wind_X: X (East) Component of the Wind Speed [m/s] | ||
22) Wind_Y: Y (North) Component of the Wind Speed [m/s] | 22) Wind_Y: Y (North) Component of the Wind Speed [m/s] | ||
23) Wind_Z: Z (Vertical) Component of the Wind Speed (postivie value is upward, away from the Earth's surface) [m/s] | 23) Wind_Z: Z (Vertical) Component of the Wind Speed (postivie value is upward, away from the Earth's surface) [m/s] | ||
24) Wind_M: Horizontal Wind Speed [m/s] | 24) Wind_M: Horizontal Wind Speed [m/s] | ||
25) Wind_D: Horizontal Wind Direction [degrees]; True Direction From Which it Blows | 25) Wind_D: Horizontal Wind Direction [degrees]; True Direction From Which it Blows | ||
26) TURB: Turbulence parameter (Eddy Dissipation Rate) based on Wing Pitot pressure [cm^2/3*s^-1] | 26) TURB: Turbulence parameter (Eddy Dissipation Rate) based on Wing Pitot pressure [cm^2/3*s^-1] | ||
27) PFlag: Wind Parameter Flag | 27) PFlag: Wind Parameter Flag | ||
28) Air_Temp_n: Air Temperature Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] | 28) Air_Temp_n: Air Temperature Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] | ||
29) MachNo_n: Mach Number based on Nose Pitot Pressure | 29) MachNo_n: Mach Number based on Nose Pitot Pressure | ||
30) IAS_n: Indicated Air Speed based on Nose Pitot Pressure [m/s] | 30) IAS_n: Indicated Air Speed based on Nose Pitot Pressure [m/s] | ||
31) TAS_n: True Air Speed based on Nose Pitot Pressure [m/s] {Calibration: slope = 16.033642 offset = 2.2182522} | 31) TAS_n: True Air Speed based on Nose Pitot Pressure [m/s] {Calibration: slope = 16.033642 offset = 2.2182522} | ||
32) TURB_n: Turbulence parameter (Eddy Dissipation Rate) based on Nose Pitot pressure [cm^2/3*s^-1] | 32) TURB_n: Turbulence parameter (Eddy Dissipation Rate) based on Nose Pitot pressure [cm^2/3*s^-1] | ||
33) Pot_Temp: Potential Temperature [K] | 33) Pot_Temp: Potential Temperature [K] | ||
34) Air_Temp2_w: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] | 34) Air_Temp2_w: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] | ||
35) Air_Temp2_n: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] | 35) Air_Temp2_n: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] | ||
36) TAS: True Air Speed based first on the Pitot Nose Pressure measurements (if available) and then on the Wing Pitot Pressure measurement [m/s] | 36) TAS: True Air Speed based first on the Pitot Nose Pressure measurements (if available) and then on the Wing Pitot Pressure measurement [m/s] | ||
37) Air_Temp: Air Temperature Corrected for Dynamic Heating based first on the Pitot Nose Pressure measurement (if available) and then based on the Pitot Wing Pressure measurement [degrees Celsius] | 37) Air_Temp: Air Temperature Corrected for Dynamic Heating based first on the Pitot Nose Pressure measurement (if available) and then based on the Pitot Wing Pressure measurement [degrees Celsius] | ||
38) TAS_Flag: True Air Speed Flag (Ones place indicates if Pitot Nose or Pitot Wing is used, Tens place indicates if Temperature Probe #1 or #2 is used) | 38) TAS_Flag: True Air Speed Flag (Ones place indicates if Pitot Nose or Pitot Wing is used, Tens place indicates if Temperature Probe #1 or #2 is used) | ||
39) TAS_X_nose: X (East) Component of the True Air Speed based on Nose Probe [m/s] | 39) TAS_X_nose: X (East) Component of the True Air Speed based on Nose Probe [m/s] | ||
40) TAS_Y_nose: Y (North) Component of the True Air Speed based on Nose Probe[m/s] | 40) TAS_Y_nose: Y (North) Component of the True Air Speed based on Nose Probe[m/s] | ||
41) Alpha_wing: Alpha (Attack) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} | 41) Alpha_wing: Alpha (Attack) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} | ||
42) Beta_wing: Beta (Sideslip) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} | 42) Beta_wing: Beta (Sideslip) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} | ||
43) Alpha: Alpha (Attack) Angle [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} | 43) Alpha: Alpha (Attack) Angle [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} | ||
44) Beta: Beta (Sideslip) Angle [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} | 44) Beta: Beta (Sideslip) Angle [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} |
Latest revision as of 16:45, 10 October 2014
1) Air_Temp_w: Air Temperature Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] 2) MachNo_w: Mach Number based on Wing Pitot Pressure 3) IAS_w: Indicated Air Speed based on Wing Pitot Pressure [m/s] 4) TAS_w: True Air Speed based on Wing Pitot Pressure [m/s] {Calibration: slope = 60.797701 offset = -150.48263} 5) Press_Alt: Pressure Altitude [m] 6) Alpha_nose: Alpha (Attack) Angle based on Nose Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} 7) Beta_nose: Beta (Sideslip) Angle based on Nose Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} 8) GS_X: X (East) Component of the Ground Speed [m/s] 9) GS_Y: Y (North) Component of the Ground Speed [m/s] 10) VERT_VEL: Vertical Velocity of the aircraft based on the change in position over a 2 seceond interval [m/s] 11) Wind_X_Nose: X (East) Component of the Wind Speed based on the Nose Probe [m/s] 12) Wind_Y_Nose: Y (North) Component of the Wind Speed based on the Nose Probe [m/s] 13) Wind_Z_Nose: Z (Vertical) Component of the Wind Speed based on the Nose Probe (postive value is upward, away from the Earth's surface) [m/s] 14) Wind_M_Nose: Horizontal Wind Speed based on the Nose Probe [m/s] 15) Wind_D_Nose: Horizontal Wind Direction from Nose Probe [degrees]; True Direction From Which it Blows 16) Wind_X_Wing: X (East) Component of the Wind Speed based on the Wing Probe [m/s] 17) Wind_Y_Wing: Y (North) Component of the Wind Speed based on the Wing Probe [m/s] 18) Wind_Z_Wing: Z (Vertical) Component of the Wind Speed based on the Wing Probe (positive value is upward, away from the Earth's surface) [m/s] 19) Wind_M_Wing: Horizontal Wind Speed based on the Wing Probe [m/s] 20) Wind_D_Wing: Horizontal Wind Direction from Wing Probe [degrees]; True Direction From Which it Blows 21) Wind_X: X (East) Component of the Wind Speed [m/s] 22) Wind_Y: Y (North) Component of the Wind Speed [m/s] 23) Wind_Z: Z (Vertical) Component of the Wind Speed (postivie value is upward, away from the Earth's surface) [m/s] 24) Wind_M: Horizontal Wind Speed [m/s] 25) Wind_D: Horizontal Wind Direction [degrees]; True Direction From Which it Blows 26) TURB: Turbulence parameter (Eddy Dissipation Rate) based on Wing Pitot pressure [cm^2/3*s^-1] 27) PFlag: Wind Parameter Flag 28) Air_Temp_n: Air Temperature Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] 29) MachNo_n: Mach Number based on Nose Pitot Pressure 30) IAS_n: Indicated Air Speed based on Nose Pitot Pressure [m/s] 31) TAS_n: True Air Speed based on Nose Pitot Pressure [m/s] {Calibration: slope = 16.033642 offset = 2.2182522} 32) TURB_n: Turbulence parameter (Eddy Dissipation Rate) based on Nose Pitot pressure [cm^2/3*s^-1] 33) Pot_Temp: Potential Temperature [K] 34) Air_Temp2_w: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] 35) Air_Temp2_n: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] 36) TAS: True Air Speed based first on the Pitot Nose Pressure measurements (if available) and then on the Wing Pitot Pressure measurement [m/s] 37) Air_Temp: Air Temperature Corrected for Dynamic Heating based first on the Pitot Nose Pressure measurement (if available) and then based on the Pitot Wing Pressure measurement [degrees Celsius] 38) TAS_Flag: True Air Speed Flag (Ones place indicates if Pitot Nose or Pitot Wing is used, Tens place indicates if Temperature Probe #1 or #2 is used) 39) TAS_X_nose: X (East) Component of the True Air Speed based on Nose Probe [m/s] 40) TAS_Y_nose: Y (North) Component of the True Air Speed based on Nose Probe[m/s] 41) Alpha_wing: Alpha (Attack) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} 42) Beta_wing: Beta (Sideslip) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} 43) Alpha: Alpha (Attack) Angle [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} 44) Beta: Beta (Sideslip) Angle [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200}