Path: Airships/Control
%vCompute the airship state vector as an acstate object from a model data structure and initial conditions of: [latitude, longitude, altitude] [airspeed, angle of attack, sideslip] [roll, pitch, yaw] -------------------------------------------------------------------------- Form: x = AirshipState( d, latLonAlt, vAB, eul ); -------------------------------------------------------------------------- ------ Inputs ------ d (.) Initial aircraft data structure, generated from "BuildAirshipModel", or you may supply just the name of an airship model. latLonAlt (4,1) Latitude (deg), Longitude (deg), Altitude (km), 4th element is Julian Date (default is JD2000) vAB (3,1) Velocity (m/s), alpha (rad), beta (rad) eul (3,1) Roll, Pitch, Yaw (rad) ------- Outputs ------- x (.) Initial aircraft state, class "acstate" --------------------------------------------------------------------------
AC: ACCoord/ECIToNED AC: ACCoord/QECI AC: ACData/ACTConstants 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: Coord/CoordinateTransform AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/EFToLatLonAlt AerospaceUtils: Coord/LatLonAltToEF 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 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: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Quaternion/Mat2Q Common: Quaternion/QMult Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Common: Transform/Eul2Q Common: Transform/IConvP Math: Linear/Cross Math: Linear/Mag Math: Linear/SkewSq Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
Back to the Airships Module page