experience and innovation

SC

Directory List

Actuator, Attitude, BasicOrbit, DemoFuns, Dynamics, Environs, Ephem, GOESData, GOESRead, GUIPlugIn, Hardware, SCData, SCDatabase, SCMat, Sensor, Demos/Actuator, Demos/Attitude, Demos/CAD, Demos/Dynamics, Demos/Environs, Demos/Ephemeris, Demos/GOESRead, Demos/GUIPlugIn, Demos/Sensor, Demos/Tutorials,

Functions and Demos

Actuator

BDDesign - Designs a blowdown system.

BloDown - Generates a blowdown curve.

CMG - Simple CMG model. Assumes a tach loop controls the CMG momentum.

Dipole - Compute the magnetic field of a dipole

EffPw - Computes the effective pulsewidth given the rise and fall times.

Friction - Computes friction torques based on a model with an exponential term.

FrictionBristle - Friction model. This model uses a bristle state.

FrictionSmooth - Rotary friction model using differentiable functions.

HydrazineThruster - Computes the thrust and fuel consumed for thrusters.

MagTorquer - Models a magnetic torquer.

MagneticTorquer - Simple MagneticTorquer model. Outputs the torque in body coordinates.

PWMSeq - Generate a pulsewidth modulated sequence given x.

RWA - A RWA model using FrictionSmooth.

RWABristle - A RWA model using FrictionBristle to model the friction.

RWASmart - Smart RWA model. This models an RWA using Hall sensors.

RWASpec - Calculates RWA parameters from spec sheet parameters.

RocketEquation - Compute the final mass from the rocket equation.

SingleAxisDrive - Model a stepping motor drive.

TorqueRod - A simple Torque rod model that uses a tanh function to model the dipole


Attitude

AddMassDot - Add mass and mass derivatives using the mass data structure.

AddSurf - Add a surface to the data structure.

AngRate - Computes the magnitude of the angular rate of the momentum vector

ArcEff - Arc efficiency from spin rate and pulsewidth.

CMGAMatrix - Computes the transfer matrix from gimbal rates to torques.

DSTCrit - Compute range of allowable initial rates for the dual spin turn

DSpnStab - Computes the dual spin stability.

DWheel - Computes the damping coefficient ratio for a damper wheel.

DblPivot - Computes the unit normal for a double pivoted assembly.

DeltaQTarget - Generate a target quaternion by limiting the total angular change.

DeltaRate - Computes the new angular rate when the inertia changes.

FAeroSurfaceAccommodation - Computes the aerodynamic force using surface accommodation coefficients.

FGravityGradientStiffness - Gravity gradient for a rigid body with small offsets from LVLH.

FPB - Integrand for pointing budgets.

GetModes - Extract flex modes from a finite element modal transformation matrix.

GimbalC - Generate gimbal commands for a gimbal stationkeeping system.

GravityGradientStiffness - Computes gravity gradient stiffness from inertia and orbit rate.

IC3X326 - Convert 3x3 inertia matrix to [Ixx Iyy Izz Ixy Ixz Iyz].

InertiaTotal - Computes the new inertia and body rate when appendages change discretely.

LibrationFrequency - Compute the libration frequency from inertia and orbit rate.

LoadFlex - Reads in flex data from a formatted text file.

MagAirC - Designs an air coil by minimizing a weighted combination of power and mass.

MagTComp - Performs a tradeoff of magnetic torquers versus thrusters.

MassProp - Compute inertia, mass and center of mass for a collection of rigid bodies.

MomArm - Computes the moment arms for a set of thrusters.

NPSPM - Computes a spin precession maneuver using a rhumb line precession.

PBudget - Computes a pointing budget over n categories.

PCentr - Calculates the time from pulse start to the controid.

PPDelay - Compute the pulse pair delay for a Spin Precession Maneuver.

PointingBudget - Creates pointing budgets using a GUI.

PrincipalAxes - Computes the principal axes for an inertia matrix.

RLP - Rhumb line precession

RLPMnvr - Simulate a rhumb line precession.

RW2SDev - Converts random walk measured over dT to standard deviation.

RYDyn - Generates open loop four channel magnitude plots for roll/yaw dynamics.

SkewDipl - Computes the skew angle for a single dipole used to control yaw and roll.

SolarF - Compute the solar force on a set of elemental areas.

SumRXF - Sum a set of torques produced by summing T = rxF

TGG - Computes a gravity gradient torque.

TRD - Computes residual dipole torques.

TRF - Computes an RF torque for a set of antenna.

TSolarP - Generates solar pressure torques with shadowing.

VXPhi - Take the cross product a matrix of vectors times a flex transformation matrix.


BasicOrbit

CP2I - Transformation matrix from the perifocal frame to the inertial frame.

E2M - Converts eccentric anomaly to mean anomaly.

E2Nu - Computes the true anomaly from the eccentric or hyperbolic anomaly.

El2RV - Converts orbital elements to r and v for an elliptic orbit.

FOrbCart - Computes the right-hand-side of the orbit equations about a mass point.

M2E - Generate the eccentric anomaly from the mean anomaly and the eccentricity.

M2EApp - Approximate root to Kepler's Equation for elliptical and hyperbolic orbits.

M2EEl - Eccentric anomaly for an ellipse.

M2EHy - Eccentric anomaly for a hyperbola.

M2Nu - Computes the true anomaly from the mean anomaly.

M2NuAbs - Computes the true anomaly from the mean anomaly without wrapping btwn -pi / pi

M2NuPb - Generate the true anomaly from the mean anomaly for a parabola.

Nu2E - Converts true anomaly to eccentric or hyperbolic anomaly.

Nu2M - Converts true anomaly to mean anomaly.

Nu2MAbs - Computes the mean anomaly from the true anomaly without wrapping btwn -pi / pi

Period - Compute the period for any orbit.

PltOrbit - Plots one orbit and the sun vector looking down on the ECI Plane.

RAEToM - Computes m, nu and E from r, a and e.

RV2A - Computes the semimajor axis given position and velocity magnitudes.

RV2El - Converts Cartesian state to Keplerian orbital elements.

RVFromKepler - Generate an orbit by propagating Keplerian elements.

VOrbit - Computes the orbital velocity.


DemoFuns

DemoController - Demo controller

DrawSCCOMETS - Draw a spacecraft. You can display planets and the sun as options.

Dyn - Returns the mass and right hand side of the dynamics equations.

DynP - Returns the mass and right hand side of the dynamics equations.

FHel - Orbit equations for InterstellarSim.

FIC - Sliding mass on a pendulum using independent coordinates

FICP - Single pendulum using independent coordinates

FMagSim - Spacecraft with 4 RWA's and 2 solar arrays.

FNLSpring - Nonlinear estimator spring model. Used by CDKFDemo.

FNMThruster - Cost functional

FRWA - Simulate a reaction wheel

FRWABristle - RWA model

FRY - Roll/yaw simulation RHS

FRYSim - Roll/yaw simulation.

FSRHS - Compute smooth friction RHS.

FTBRef - Right hand side of the two body equations.

HNLSpring - Nonlinear estimator measurement spring model

HRY - Measurement equation for a roll/yaw controller.

KConst - The constraint equations and Jacobians. The outputs are

KConstP - The constraint equations and Jacobians. The outputs are

KConstQ - The constraint equations and Jacobians. The outputs are

QMultJPL - Q2 transforms from A to B and Q1 transforms from B to C


Dynamics

ASim - Attitude simulation of a rigid body.

DIModel - Double integrator model.

FAKM - AKM Burn right-hand-side

FDC - The right hand side of equations formulated using Lagrange multipliers

FGs - Gyrostat right-hand-side.

FPivot - Computes the right hand side of the spacecraft with pivot eofm.

FRB - Rigid body right-hand-side.

FRBWRIG - Simulates a spacecraft with rate integrating gyros.

FRBWithMag - Rigid body right-hand-side with magnetic torque computed internally.

FTB - Two body spacecraft model right-hand-side.

FXModel - Plant for a momentum bias spacecraft with flexible solar arrays.

GSModel - Gyrostat dynamics model which computes acceleration or plant matrices.

GetFlex - Reads in flex data from a formatted text file. See also LoadFlex.

MBModel - Computes the state space description of a momentum bias spacecraft

PlotFlex - Plots the flex model including the mode shapes.

RBModel - Computes the angular acceleration of a rigid body.

SCWithRollPivot - Model for a spacecraft with a roll pivot.

SCwPivot - Model for a spacecraft with a single pivoted momentum wheel.

TBModel - Models two rigid bodies attached by a 1 to 3-dof hinge.

Tree - Right hand side of the equations of motion for a topological tree.

TreeAdd - Add a body to the tree data structure.

TreeH - Computes the momentum for the topological tree dynamics.

TreeInit - Create the tree data structure

TreePlot - Plot the output of tree.

TreePrnt - Print out the body information for the tree model.

VIModel - Computes the angular acceleration of a body with time varying inertia.

WireC - The right hand side of the wire equations formulated using Lagrange multipliers

WireDMch - Models the deployment mechanism

WireFRB - Spacecraft with multiple wires

WireH - Magnitude of the angular momentum

WireInit - Initialize the wire model data structures

WirePlot - Plot the wires. One wire is plotted on each page.


Environs

AtmDens1 - Computes the atmospheric density using an exponential model.

AtmDens2 - Computes the Earth's atmospheric density using scale heights.

AtmDensMars2 - Computes the atmospheric density of Mars.

AtmJ70 - Computes the atmospheric density using Jacchia's 1970 model.

AtmSnd - Computes the speed of sound in the atmosphere.

AtmTemp - Computes the atmospheric temperature using a simplified model.

BDipole - Computes the geocentric magnetic field based on a tilted dipole model.

BMF - Magnetic field based on the Mead-Fairfield Model

BaromExp - Computes the barometric exponent.

DiffusionExp - Computes the diffusion exponent.

Disturbances - Compute the total force and torque on a spacecraft generated

EarthAlb - Computes the heat absorbed per unit area due to albedo.

EarthRad - Computes the heat absorbed due to earth radiation.

Geo - Computes parameters for a geosynchronous orbit.

GeoEclps - Computes the normalized sun intensity for an earth geosynchronous orbit.

MagField - Computes the magnetic field using the DGRF/IGRF model.

MagFieldPlanet - Computes the magnetic field using Schmidt normalized coefficients.

MagneticDipole - Computes the magnetic field of a dipole along the z axis.

MagneticDipoleCart - Computes the magnetic field of a dipole along m.

MolWt2R - Computes R given the molecular weight.

PlanetaryAtmDens - Computes the atmospheric density for Earth, Mercury, Venus, Mars and Pluto.

PlanetaryRadiationAndAlbedo - Computes the albedo and radiation flux for planets.

ReadMagField - Read in the magnetic field in the form:

SolarFluxPrediction - This function computes the solar flux prediction based on Julian date.

SolarFlx - Solar flux from the sun as a function of distance in AU.

TerrestrialSolarFlux - Solar flux from the sun with seasonal variation.

TitanAtmosphere - Titan density model.

Water - Properties of water.


Ephem

CEcl2Eq - Transformation matrix from ecliptic to Earth equatorial planes.

DMS2Deg - Convert degrees, minutes and seconds to radians

DMS2Rad - Convert degrees, minutes and seconds to radians

Deg2DMS - Convert degrees to degrees, minutes and seconds.

Deg2HMS - Convert radians to hours, minutes and seconds

DeltaML - Compute total change in longitude between two orbits.

ECIToECIR - Computes the transformation form ECI to ECIR.

ECIToPlanet - Computes the matrix from mean of Aries 2000 to planet fixed frame.

EOfE - Computes the equation of the equinoxes

EarthNut - The matrix that rotates from the Earth mean axes to the true axes

EarthPre - Computes the earth precession matrix

EarthRot - Computes the earth greenwich matrix that transforms from ECI to earth fixed.

EarthRotationZero - Determine jD for when the earth-fixed frame is aligned with the ECI frame.

EarthRte - Computes the mean earth rate.

Eclipse - Computes eclipses.

EclipseDuration - Computes eclipse orbit fraction.

FSolstice - RHS for computing solstice.

GASTime - Compute Greenwich apparent sidereal time.

GMSTime - Compute Greenwich mean sidereal time from Julian date.

GTrack - Draws a ground track on an ellipsoid.

HMS2Deg - Convert hours, minutes and seconds to degrees.

HMS2Rad - Convert hours, minutes and seconds to radians.

HMS2S - Converts hours, minutes and seconds into seconds

InterpolateState - Interpolate a planet's state for a given Julian Date.

LagrangePointsL1ToL5 - Computes the position of Lagrange points in normalized rotating coordinates

LoadFK5 - Reads in the FK5 catalog in MICA format.

MSidDay - Computes a mean sidereal day

MSolDay - Computes a mean solar day.

MarsRot - Computes the matrix that transforms from ECI to areographic axes.

MoonEl - Computes the moon orbital elements with respect to the earth inertial frame.

MoonRot - Computes the matrix that transforms from ECI to selenographic axes.

MoonV1 - Generate the moon vector in an earth or spacecraft centered frame.

MoonV2 - Generate the moon vector in an earth or spacecraft centered frame.

Moons - Lists moons of a planet or planet center about which a moon orbits.

NutDelta - The changes in longitude and obliquity due to earth nutation

ObOfE - Computes the mean obliquity of the ecliptic of date

Parallax - Computes the parallax of a target when viewed by an observer

PlanetPosJPL - Get positions for an array of planets using the JPL ephemeris.

PlanetPosition - The position vectors, gravitational parameters and velocity for the planets.

PlanetaryDistanceToSun - Finds the distance to the sun and the solar flux.

Planets - Functions for the orbital elements of the planets in the heliocentric frame.

QSpin - Creates a series of quaternions with its x axis spinning about u.

QSunNadir - Compute the sun-nadir quaternion and other quantities.

QSunPointing - Creates a sun reference frame with +x pointing at the sun.

RSHMoon - Generates a topographic map of the moon using spherical harmonics.

Rad2DMS - Convert radians to degrees, minutes and seconds

Rad2HMS - Convert radians to hours, minutes and seconds

S2HMS - Converts seconds into hours, minutes and seconds

SolarSys - Computes the position vectors of the planets as a function of time.

SolarSysJPL - Computes the position vectors of the planets as a function of time.

SolarSystemElements - Computes the solar system elements on a given Julian Date.

SolarSystemProperties - Look up a moon or planet and return its properties.

SolarVisibility - Compute the solar intensity experienced by a spacecraft.

SortFK5 - Sort FK5 by distance in light years and save in a new file

StarMap - Draws a star map.

SunNadir - Compute the sun-nadir angles and yaw rate.

SunV1 - Generate the sun vector in the earth-centered inertial frame. Will

SunV2 - Moderate precision sun model.

SunVectorECI - Finds the sun vector any place in the solar system

TransformLagrangePoints - Computes the position and velocity of stable Lagrange points.

TruEarth - Computes the matrix from mean of Aries 2000 to earth fixed frame.

UVAA - Apparent sun vector from quantities tabulated in the astronomical almanac.


GOESData

G0758910.BIN;1 - Example GOES data.

SATPOS.TXT;1 - Satellite positions.


GOESRead

BHarm - Computes a sine/cosine harmonic series for the magnetic field.

BTrans - Transforms the GOES data into popular earth pointing frames.

GOESCD - Ordering information for the GOES CD-ROM.

GOESLeg - Draws the GOES Legend.

GOESLon - Computes the west longitude of a GOES spacecraft.

Glitch - Removes glitches from data. If bMax is omitted it will look for

LoadGOES - Loads GOES binary data. Will edit out magnetometer glitches.

LoadMag - Loads GOES magnetometer data. This can take a lot of data. It uses the

LoadSatP - Loads in GOES Satellite Positions

LoadSers - Loads GOES data from multiple files. Similar to LoadMap only returns

TwoC2F - Converts two's complement of length 2b to a floating point number.

WeathLeg - Draws the Weather Legends.

Weather - Loads GOES binary data. Will edit out magnetometer glitches.


GUIPlugIn

AttitudeProfilePlugIn - Generate attitude profiles.

CommandPlugIn - Create a command interface for a simulation.

DrawSCPlugIn - Draw spacecraft in orbit about a planet.

ElementsPlugIn - Create an orbit elements GUI plug in.

GUICounter - This gui displays a counter.

OrbitDisplayPlugIn - Create an orbit display. To initialize type:

ParseCommand - Parse a command string

PlotPlugIn - Plot a variable number of points. The function is called as:

PlugInDemo - Demonstrate using the GUI plug ins with an orbit simulation.

SpacecraftStatePlugIn - Create an spacecraft state GUI plug in.


Hardware

FloatToWord - Convert floating point to word.

HMagEl - Computes the magnetic field for a filament or loop magnetic element.

PivotMch - Models a pivot mechanism and converts stepping motor steps to pivot angle.

WordToFloat - Convert an integer word to a floating point number.


SCData

AutoCADColors.txt - Generate colors for AUTOCAD.

BRIGHT.CAT - Bright star catalog.

CLIPPER.dxf - Pan am space clipper.

Commands.txt - Commands

ComstarSA.txt - Comstar solar array

FK5.100 - FK5 catalog.

HUBBLE.dxf - Hubble space telescope.

PolylineTest.dxf - Polyline file.

TFIGHTER.dxf - Tie like fighter.

USS_LA.dxf - US submarine.

cassini.dxf - Cassini CAD Model

gltm2b.topo - Topographic data

probe.dxf - Huygens CAD model.

sCTConstants.mat - Constant database.

sts.txt - Shuttle NORAD 2 line elements.

visual.txt - Visible satellite NORAD 2 line elements

zvezda1.dxf - Zvezda module.


SCDatabase

ScDB - Outputs the value of a constant for the spacecraft.


SCMat

Ariel.mat - Texture map.

COMETS_Data.mat - Comets spacecraft CAD data.

Callisto.mat - Texture map.

CassiniColor.mat - Cassini model colored.

Charon.mat - Texture map.

ComStarI.mat - ComStar inertia data.

CubeSat.mat - Data for a simple satellite with thrusters.

Deimos.mat - Texture map.

Dione.mat - Texture map.

DistModl.mat - Disturbance model data.

EarthHR.mat - Texture map.

ElementSet.mat - Orbital element set

Enceladus.mat - Texture map.

Europa.mat - Texture map.

FlexM00.mat - Flex model, array at 0 deg.

FlexM90.mat - Flex model, array at 90 deg.

Ganymede.mat - Texture map.

Huygens.mat - Spacecraft CAD model.

Iapetus.mat - Texture map.

Jupiter.mat - Texture map.

MagData.mat - Magnetic field data.

Mars.mat - Texture map.

Mercury.mat - Texture map.

Mimas.mat - Texture map.

Miranda.mat - Texture map.

Moon.mat - Texture map.

Neptune.mat - Texture map.

Oberon.mat - Texture map.

Phobos.mat - Texture map.

Pluto.mat - Texture map.

Proteus.mat - Texture map.

RYC.mat - Roll/yaw control data.

Rhea.mat - Texture map.

Saturn.mat - Creates the rings of Saturn.

ShuttleModel.mat - Shuttle CAD database.

SolarFluxPredictions.mat - Solar flux data.

Sun.mat - Texture map.

Tethys.mat - Texture map.

TitanDensityData.mat - Data for Titan atmosphere density.

Titania.mat - Texture map.

Triton.mat - Texture map.

Umbriel.mat - Texture map.

Uranus.mat - Texture map.

Venus.mat - Texture map.

XYZSat.mat - Simple spacecraft with axes.

planet.mat - Planet file


Sensor

AI2Rate - Converts attitude increments to rate.

Accel - Models accelerometers. This model includes quantization, noise and a bias.

CW2Roll - Converts the output from a conical scanning sensor to roll. Gives two

Counter - Simulate a counter.

Diffraction - Computes the point spread function as a function of unit vector

ESA - Simulates an ideal earth sensor. This generates roll and pitch angles based

ESACS - Models a conical scanning earth sensor. The noise is added to

ESAChord - Compute the delta earth chord for a scanning earth sensor.

EarthSensorScanning - Model a scanning earth sensor.

EnergyPerRing - Gives the energy per ring and diameter of the each ring for a

FP2RADec - Converts focal plane coordinates into right ascension and declination of the

FPSensors - Computes the output of focal plane sensors.

FSDG - Gyro right-hand-side .

Gyro - Models a gyro. input is a data structure with, at a minimum,

GyroData - Typical gyro noise data. The gyro noise model is:

HRG - Model a hemispherical resonating gyro. Includes all noise sources

HSAData - Computes the hsa sensor data for a spinning spacecraft. This computes

HSAPlot - Plots the HSA sensor data.

LightDetectorIntegrals - Gives the normalized stellar-light detector integral given

Magnetometer - Magnetometer model. Outputs the b field in body coordinates.

Nadir - Computes nadir angle from a cant angle, earth angle and chordwidth

Optic2D - Models a generic 2 dimensional optical sensor.

PointSpreadFunction - Computes the point spread function as a function of u for a circular

QProp - QProp propagates a quaternion based on updated angular increment measurements.

RADec2FP - Converts right ascension and declination into focal plane coordinates.

RIGModel - Computes the output of a rate integrating gyro package.

RIGOut - RIG output.

RWACountToRate - Converts RWA tachometer count to rate.

RateGyro - Model a rate gyro. Includes all noise sources

RelativePositionSensor - Model for a relative orbital position sensor. This is a combination

SCClock - Models a spacecraft clock.

SDG - Single degree of freedom mechanical gyros.

SSA - Simulates a single axis suns sensor

SSEye - Given the equation m = a(1)*x^1 + a(2)*x^2 +...

StarTracker - Simple star tracker model. You can get the default parameters by

SunSensor - Model a sun sensor.

U2FP - Computes the location in the focal plane of unit vectors.

U2Pix - Converts a unit vector into a pixel location. u(3) must be > 0 to be


Demos/Actuator

BristleFrictionSim - Demonstrate the bristle friction model with a velocity ramp.

CMGDemo - Demonstrate the use of CMGs. Shows how to use a pseudo inverse to distribute

PivotDemo - Simulates a pivot rotation. The pivot is rotated in two steps. The steps

RWABristleSim - Test the reaction wheel model with bristle friction

RWADemo - Demonstrate different RWA models.

RWASim - Simulate a RWA with a PI rate controller.

RWASmartSim - Test the smart reaction wheel model.

SmoothFrictionDemo - Demonstrate the use of the smooth friction model


Demos/Attitude

Attitude3D - Simple sim using a CAD model of the spacecraft to view the attitude.

GimbalControl - Tests a gimbaled thruster stationkeeping control system. This is the type

JitterDemo - Displays different kinds of jitter.

MagneticControlSim - Demonstrates magnetic control.

REAControl - Implements a thruster control system. Uses a CAD model of the spacecraft.

RollYawControl - This script explores different roll/yaw controllers.

SCTTutorial - Implements a spacecraft control tutorial.

TPDRes - Study pulse resolution. Demonstrates using a multirate system and dither


Demos/CAD

BuildCADModelDemo - Build a solar sail model using BuildCADModel.

BuildCassini - Demonstrate how to create a CAD model from a .dxf file.

BuildCubeSat - A very simple spacecraft with thrusters and one sensor.

BuildDXF - Loads in dxf data for Cassini and Huygens, and saves data to mat-files.

BuildMAP - Build a model of the Microwave Anisotropy Probe.

BuildPlutoProbe - A very simple spacecraft with thrusters and one sensor.

BuildRecon - Draw a picture of the recon satellite.

BuildSC - Build up a picture of a geosynchronous communications satellite.

BuildShuttle - Build a shuttle model

BuildSimpleSat - A very simple spacecraft with one sensor.

BuildXYZSat - A very simple 'XYZ' spacecraft with six panels and axes.

CADColorDemo - Demonstrate CADColor

CassiniColorDemo - Demonstrate CADColor using the Cassini orbiter.

CassiniSim - Draws a picture of the Cassini orbiter, Huygens probe, Saturn, and Titan.

DisturbanceFlatPlate - Disturbance analysis with two thin plates. Change m.mass.cM to move the

DisturbanceModel - A Disturbance model. All units are in meters.

GOESModel - Make a model of the GOES spacecraft

NEPModel - Build a nuclear electric vehicle using BuildCADModel

SCDisturb - Demonstrate how to use the disturbance modelling function with CAD models.

ShuttleSim - Simulate the space shuttle model.


Demos/Dynamics

ConstDyn - Example 4.2 and 4.3 in the reference. We are using RK4 for this

NutationAnimation - Demonstrates rigid body rotation.

NutationSim - Demonstrates nutation and generates an STK attitude file.

RobotArm - Six body simulation of a spacecraft with a robot arm.

TTB - Demonstrate two body dynamics using the two body dynamics model.

TreeCAD - Three body simulation with initialization using the CAD tools.

TreeSim - Three body simulation. The bodies are connected

WireSimG - This script demonstrates the deployment of the wire from the


Demos/Environs

J70Demo - Demonstrate the J70 atmosphere model.

J70SunDemo - Demonstrate the J70 atmosphere model.

MagneticField - Test the magnetic field.


Demos/Ephemeris

JPLPlanetDemo - Demonstrate JPL ephemeris for the solar system.

TEarth - Demonstrate earth nutation, precession and rotation.

TEclipse - Computes eclipses.

TPlanets - Demonstrate the planets model.


Demos/GOESRead

GOESDemo - Demonstrates the GOES Toolbox functions.


Demos/GUIPlugIn

CommandPluginDemo - Demonstrate command lists

LaunchGUIDemo - Launch the GUI plug in demo. See the GUIPlugIn folder for the function.

TelemetryPlotDemo - Demonstrate real-time plots using TelemetryPlot.


Demos/Sensor

GyroDemo - Test the gyro model. First runs the model with the default RIG, RG, FOG

TGyro - Simulate various single degree of freedom gyros.


Demos/Tutorials


SVN Revision: 10554


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