Missions Module

Directory List

Comsat ComsatData Demos/Comsat
Demos/FastReorientation Demos/SpaceStation Demos/SunNadir
FastReorientation SpaceStation SunNadir


Comsat

Generates the data needed for a attitude data collection in TrnsfOrb.m
The ComStar satellite properties database GUI.
Simulate a dual-spin-turn.
Generates the data needed for a dual spin turn in TrnsfOrb.m
Generates the data needed for a delta Vs in TrnsfOrb.m
Updates the fuel mass.
Gets HSA attitude data
Computes the half system moment arms
Generates the data needed for an injection in TrnsfOrb.m
Generates the data needed for initialization in TransferOrbit.m
Count the number of odd and even numbered thrusters in use.
Updates orbital elements based on an impulsive delta-V
Kalman Filter for pitch
Design the Pitch Loop including a tach loop for the wheel.
Computes the REA and tank pressure
Computes the thrust and fuel consumed for thrusters.
Designs the dual-spin-turn roll estimator
Generates the data needed to compute stationkeeping maneuvers
Computes spin precession maneuver data for fuel budgets
Generates the data needed for an SPM maneuver in TrnsfOrb.m
Performs a spin precession maneuver.
Find the surfaces that are in shadow.
Simulates a spin change.
Computes spin precession maneuver data for fuel budgets
Generates the data needed for a spin change in TrnsfOrb.m
Estimates rate from measurements of period
Computes the thrust level of a set of thrusters.
Computes the thruster torques based on exponential rise and fall time model.
Simulates transfer orbit
ComStarI.matComStar inertia data.
DistModel.matComsat disturbance model data.
NoiseF.matComsat noise filter matrices
PMWA.txtComsat MWA controller matrices.
RYC.matComsat roll/yaw control data.

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ComsatData

ComStarI.matComStar inertia data.
DistModel.matComsat disturbance model data.
NoiseF.matComsat noise filter matrices
PMWA.txtComsat MWA controller matrices.
RYC.matComsat roll/yaw control data.

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Demos/Comsat

Simulate the AKM firing for the ComStar spacecraft.
The acquisition sequence for the ComStar satellite.
Generates the mass properties for the ComStar demo satellite.
Simulate the ComStar dual spin turn.
Computes the total disturbance torque for the ComStar satellite.
Designs earth sensor noise filters for the ComStar satellite.
Demonstrate a pointing budget for a typical satellite.
Design a PD controller for pitch for the ComStar satellite.
Tests the MWA pitch loop for the ComStar satellite.
Design and test the low frequency roll/yaw control system.
Design and test the nutation compensator.
Compensate the flexible solar array on the ComStar Spacecraft.
Simulate a spin precession maneuver for ComStar.
Demonstrate the automatic spin up for ComStar.
Simulates transfer orbit for ComStar.
Analyze the flexible solar array on the ComStar Spacecraft.
Design a roll/yaw controller using a double pivot

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Demos/FastReorientation

Simulate the fast reorientation system.
Simulate the fast reorientation system and demonstrate quaternion propagation

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Demos/SpaceStation

Momentum unloading with magnetic torque
Design a manufacturing space station
Space Station Attitude Control
SpaceStationProps.matStation geometry properties for disturbance analysis.

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Demos/SunNadir

Implements and simulates Sun nadir pointing control.

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FastReorientation

Executes the fast reorientation system slew maneuver.
Plans the fast reorientation system slew maneuver.
Propagates the target profile for the fast reorientation slew maneuver.
Compute the target quaternion for the fast reorientation system.
Calculates the torque for the fast reorientation system slew maneuver.

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SpaceStation

Right-hand-side for attitude and orbit of spacecraft.
Implements the space station control system
Calculates drag for the LEO space station

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SunNadir

Control demand distribution
Transform core frame to solar array frame
Transform sun vector from I frame to body frame
Initial quaternion and solar array angle given the sun geometry.
Spacecraft sun-nadir RHS with 4 RWA's and 2 solar arrays.
Transform a vector from the sun sensor frame to the core frame
Creates a small angle transformation matrix.
Sun sensor attitude determination for sun-nadir pointing.
Models the output for array mounted analog sun sensors.
Compute the orbit right ascension angle

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