Path: AC/ACDemoFuns
% Provide a default aircraft state.
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Form:
x = DefaultACState;
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Inputs
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None
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Outputs
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x Aircraft state vector, consisting of:
- r (3,1) ECI position vector
- q (4,1) Quaternion from ECI to body
- w (3,1) Inertial body rate in body frame
- v (3,1) Velocity of cm wrt air
- wR (:,1) Angular velocity of rotors
- mass (1,1) Mass
- inertia (6,1) Inertia
- cG (3,1) Center of mass
- engine (:,1) Engine states
- actuator(:,1) Actuator states
- sensor (:,1) Sensor states
- flex (:,1) Flex model states
- disturb (:,1) Disturbance model states
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AC: ACCoord/ECIToNED AC: ACCoord/VTToVB 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 Common: Quaternion/Mat2Q Common: Quaternion/QMult Common: Transform/Eul2Q
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