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Airbreathing, Help, Hypersonic, LVData, LVModels, LaunchSim, Missile, MultiStage, Utilities, Demos/Airbreathing, Demos/LVModels, Demos/MultiStage,
EngineDataFromTable - Generate engine data from a table.
EngineExample - Example engine parameters. Returns a data structure.
EngineTable - Generate an engine table. Each row is an altitude and each
MixedFlowTurbofan - Mixed flow turbofan engine performance.
MixedFlowTurbofanProfile - Mixed flow turbofan engine performance profile for p, h and v.
Ramjet - Ramjet model including aerodynamic losses.
RamjetH2 - Ramjet model including aerodynamic losses. The default fuel is H2.
TurboRamjetSim - Simulates a turboramjet engine on a fixed flight path angle trajectory.
Turbofanramjet - Models a turbofanramjet.
FileHelp - View the file headers.
NewtonianAeroPropertiesFromOBJFile - Computes the normal coefficient of a body in hypersonic flow
NewtonianLD3D - Newtonian lift and drag for hypersonic flight in a standard atmosphere.
FMinTOrbitInjection - Function to be minimized by fmins for MinTOrbitInjection.
LaunchParamToEl - Converts flight path angle, velocity and r to orbital elements.
LaunchVehicle2D - The right hand side of a 2D launch model.
LaunchVehicle3D - Compute position, velocity and mass derivatives for a launch vehicle.
LiftAndDragSeaLevelToOrbit - Two dimensional lift and drag.
LiftingReentry3D - Compute position, velocity and mass derivatives for a launch vehicle.
MinTOrbitInjection - Constant thrust minimum time orbit injection.
OptimizeTSTO - Comment.
RHSMinTOrbitInjection - RHS for planar equations.
RHSRigidBody - Compute position, velocity and mass derivatives for a launch vehicle.
RHSTSTO - Compute position, velocity and mass derivatives for a launch vehicle.
Reentry - Non dimensional reentry dynamics model.
ReentryPlot - Plot values from reentry simulations.
SolidRocketInertia - Computes the inertia and inertia derivative for a solid rocket.
TSTOOptimization - Size a horizontal launch/horizontal landing two stage to orbit vehicle.
TSTOSizing - Size a horizontal launch/horizontal landing two stage to orbit vehicle.
GuidedLaunch2D - Compute the parameters to perform a 2D launch into a circular orbit.
GuidedLaunch2DCost - Cost function for the 2D launch.
GuidedLaunch2DRHS - The right hand side of a guided 2D launch model.
GuidedLaunch2DSim - Simulates a 2D guided launch.
GuidedLaunch3D - Simulate a guided launch to LEO.
GuidedLaunch3DRHS - Compute position, velocity, mass derivatives for guided launch to orbit
IncLatVelToAzimuthHeading - Compute azimuth and heading req.d at lat. and V to reach inclination.
LSQLaunch - Use least squares approach to compute launch conditions
LSQLaunchSim - Simulate launch trajectory given initial parameters, return final states
LaunchGUI - Select a launch vehicle, set initial conditions, simulate 2D launch.
LaunchOptions - Specify the options for a launch simulation.
LaunchSummary - Print out summary of launch data. For use with GuidedLaunch2D.
LaunchTime - Compute the time until launch, given launch site and desired orbit.
RHSRocket2DPointMass - Simulate the controlled trajectory of a point mass aircraft model.
RocketSim - Simulates a Rocket flight
StageTimes - Compute the ignition and burnout times given stage mass histories.
MissileDistance - Compute the min angular distance (around the Earth) that connects 2 pts
MissileLambert - Find initial velocity and flight path angle that gives desired distance
MissileMaxRange - Compute the maximum range for a missile given its initial velocity.
MissileTrajAnalysis - Analyze the trajectories for around-the-Earth missile launches.
MissileVelocity - Compute initial velocity and flight time for a missile trajectory
BurnoutVelocity - Compute the burnout velocity for a multi-stage rocket
EP2M - Converts structural and payload ratios into masses.
EPPS - Payload and structural mass ratios for parallel stages.
M2EP - Converts masses to structural and payload ratios.
M2MS - Converts total, final and payload masses to stage masses and ratios.
MS2M - Converts stage and payload masses to total masses and final masses.
MSData - Complete the stage data for a multi-stage missile.
MSTOR - Computes the multistage tradeoff ratios.
MSVRatio - Compute the velocity ratio for a multi-stage rocket
OptimalPayloadRatio - Compute the optimal payload ratios for a multi-stage rocket.
RemoveStage - Remove a stage from a multi-stage data structure.
RocketDatabase - Load the properties for a rocket: mS, thrust, ISP, exhaust velocity.
SS2O - Compute the fuel mass needed to reach a velocity given mass properties and ISP.
ScaleVehicle - Scale a vehicle's properties.
WriteEngineData - Generate engine data from a table.
F135Engine - Model of the Pratt & Whitney F135 Engine.
GenerateEngineTables - Generate ramjet and turbofan data.
LiftAndDragForReentryVehicle - Compute lift and drag coefficients for a reentry vehicle.
RamjetDemo - Demonstrate a ramjet.
SteadyClimb - Simulate a steady climb.
ISSMission - Explore different launch vehicles for an ISS orbit
LaunchSimulation - Launch vehicle simulation.
LiftAndDragForMissile - Compute lift and drag coefficients for a missle.
LiftingReentrySimulation3D - Reentry simulation.
ReentryCartSimulation - Reentry simulation.
ReentrySimulation - A simulation of reentry.
SSTO3DLaunchSimulation - Launch vehicle simulation for an SSTO vertical launch.
SSTOLaunchSimulation - Launch vehicle simulation for an SSTO vertical launch.
SolveGravityTurn - Solve for the initial conditions to perform a gravity turn trajectory.
TSTODemo - Demo a horizontal launch/horizontal landing two stage to orbit vehicle.
TSTOSimulation3D - End-to-end TSTO launch simulation.
StructuralFractionSSTO - Compute the payload fraction as a function of structural fraction.
TLunarT - Plan a simplified lunar transfer assuming you start in a geo transfer orbit.
SVN Revision: 23297
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