Path: ACPro/ACPerformance
% Computes the rate of climb and acceleration. Since version 3 (ACT). -------------------------------------------------------------------------- Form: [rateOfClimb, accel] = RateOfClimb( d, velocity, altitude ) -------------------------------------------------------------------------- ------ Inputs ------ d (1,1) See "ConcordeProperties.m" velocity (1,:) Velocity altitude (1,:) Altitude (m) ------- Outputs ------- rateOfClimb (1,:) Range (m/s) accel (1,:) Acceleration (m/s^2) -------------------------------------------------------------------------- Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance," Cambridge, pp. 271-272. --------------------------------------------------------------------------
ACPro: ACPerformance/ConcordeProperties Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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