Path: ACPro/ACPerformance
% Computes the rate of climb and acceleration.
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Form:
[rateOfClimb, accel] = RateOfClimb( d, velocity, altitude )
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Inputs
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d (1,1) See "ConcordeProperties.m"
velocity (1,:) Velocity
altitude (1,:) Altitude (m)
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Outputs
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rateOfClimb (1,:) Range (m/s)
accel (1,:) Acceleration (m/s^2)
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Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance,"
Cambridge, pp. 271-272.
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ACPro: ACPerformance/ConcordeProperties ACPro: ACProAerodynamics/ConcordeLD AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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