AirshipTrim:
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Compute the trim controls for an airship at a given flight condition.
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Form:
[T,mu,dElv] = AirshipTrim( d, h, theta, alpha, V );
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Inputs
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5 INPUTS:
d (.) Airship model data structure
h (1) Altitude [m]
theta (1) Pitch angle [rad]
alpha (1) Angle of attack [rad]
V (1) Total velocity [m/s]
OR
2 INPUTS:
d (.) Airship model data structure
x (.) Aircraft state object [m]
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Outputs
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T (1) Trim thrust value [N]
mu (1) Trim thrust pitch angle [rad]
dELV (1) Trim elevator deflection [rad]
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Copyright 2003 Princeton Satellite Systems, Inc.
All rights reserved.
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Children:
AC: ACCoord/AlphBeta
AC: ACCoord/ECIToNED
AC: ACCoord/QECI
AC: ACDynamics/AC
AC: ACDynamics/ACInit
AC: Classes/@acstate/abs.m
AC: Classes/@acstate/acstate.m
AC: Classes/@acstate/get.m
AC: Classes/@acstate/length.m
AC: Classes/@acstate/minus.m
AC: Classes/@acstate/mrdivide.m
AC: Classes/@acstate/mtimes.m
AC: Classes/@acstate/plus.m
AC: Classes/@acstate/subsasgn.m
AC: Classes/@acstate/subsref.m
AC: Classes/@acstate/zeros.m
AeroUtils: AtmosphericCalculations/AirData
Airships: Mass/BuildAirshipMassModel
Airships: Modeling/BuildAirshipModel
Airships: Simulation/AirshipAero
Common: Atmosphere/StdAtm
Common: Quaternion/Q2Eul
Common: Quaternion/QMult
Common: Quaternion/QPose
Common: Transform/Altitude
Common: Transform/IConvP
Math: Linear/Mag
