Path: Airships/Control
% Compute a linearized model of an airship at a given flight condition. -------------------------------------------------------------------------- Form: g = AirshipLinMod( d, h, theta, alpha, V ); -------------------------------------------------------------------------- ------ Inputs ------ 4 INPUTS: d (.) Airship model data structure h (1) Altitude [m] theta (1) Flight path 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] ------- Outputs ------- g (.) State-space data structure -------------------------------------------------------------------------- Copyright (c) 2003 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
AC: ACCoord/AlphBeta AC: ACCoord/ECIToNED AC: ACCoord/QECI AC: ACData/ACTConstants 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 AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AirData AerospaceUtils: Coord/CoordinateTransform AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/EFToLatLonAlt AerospaceUtils: Coord/LatLonAltToEF AerospaceUtils: Coord/QIToBDot Airships: Control/AirshipTrim Airships: Mass/AirshipMassModel Airships: Mass/BuildAirshipMassModel Airships: Mass/IntegrateMassProps Airships: Modeling/AddedMass Airships: Modeling/AirshipCV Airships: Modeling/AirshipCoefficients Airships: Modeling/AirshipGeometry Airships: Modeling/AirshipInertiaFactors Airships: Modeling/AirshipIntegrals Airships: Modeling/BuildAirshipModel Airships: Modeling/FinFactors Airships: Modeling/FinGeometry Airships: Modeling/GondolaGeometry Airships: Modeling/HalfEllipsoid Airships: Simulation/AirshipAero Airships: Simulation/AirshipInit SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/TruEarth SC: SCData/sCTConstants Common: Atmosphere/StdAtm Common: Classes/@statespace/and.m Common: Classes/@statespace/close.m Common: Classes/@statespace/connect.m Common: Classes/@statespace/eig.m Common: Classes/@statespace/get.m Common: Classes/@statespace/getabcd.m Common: Classes/@statespace/getsub.m Common: Classes/@statespace/isempty.m Common: Classes/@statespace/mtimes.m Common: Classes/@statespace/plus.m Common: Classes/@statespace/series.m Common: Classes/@statespace/set.m Common: Classes/@statespace/statespace.m Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Control/Append Common: Control/C2DZOH Common: Control/Parallel Common: Control/Series Common: Control/SizeABCD Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Quaternion/Mat2Q Common: Quaternion/Q2Eul Common: Quaternion/Q2Mat Common: Quaternion/QForm Common: Quaternion/QMult Common: Quaternion/QPose Common: Quaternion/QTForm Common: Quaternion/QUnit Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Common: Transform/Altitude Common: Transform/Eul2Q Common: Transform/IConvP Common: Transform/Mat2Eul Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/SkewSq Math: Linear/SkewSymm Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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