Path: Airships/Simulation
% Sensor model for airship.
Outputs are
roll rate (rad/sec)
pitch rate (rad/sec)
yaw rate (rad/sec)
axial velocity (m/s)
lateral velocity (m/s)
normal velocity (m/s)
angle of attack (rad)
sideslip angle (rad)
roll angle (rad)
pitch angle (rad)
yaw angle (rad)
altitude (m)
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Form:
g = AirshipSensor( x, d, opt )
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Inputs
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x (:) acstate data structure
d (:) Aircraft data structure
opt 'rhs' outputs state derivatives
'meas' outputs measurements
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Outputs
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g (:) Sensor output
.p (1,1) Roll rates
.q (1,1) Pitch rate
.r (1,1) Yaw rates
.u (1,1) Axial velocity
.v (1,1) Lateral velocity
.w (1,1) Normal velocity
.alpha (1,1) Angle of attack
.beta (1,1) Sideslip Angle
.phi (1,1) Bank Angle
.altitude (1,1) Altitude
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AC: ACCoord/AlphBeta AC: ACCoord/ECIToNED AC: ACCoord/EulNED Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Quaternion/Mat2Q Common: Quaternion/Q2Eul Common: Quaternion/Q2Mat Common: Quaternion/QMult Common: Quaternion/QPose Common: Transform/Altitude Common: Transform/Mat2Eul Math: Linear/Mag
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