Tas Input Not Optimized For Mac
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. Speed of sound less than 200 m/s or greater than 350 m/s. Static pressure less than 1000 Pa or greater than 106,500 Pa. Using the Table Lookup method in these instances causes inaccuracies. Equation Compute output airspeed directly using block input values TAS, a, and P 0.
Tas Input Plugin
Calculations involving supersonic airspeeds (greater than Mach 1) require an iterative computation. If the function does not conclude within 30 iterations, it displays an error message. The Ideal Airspeed Correction block automatically uses the Equation method for any of these instances.