Package gov.nasa.jpl.aerie.foomissionmodel.activities

Class SolarPanelNonLinear

java.lang.Object

gov.nasa.jpl.aerie.foomissionmodel.activities.SolarPanelNonLinear

public final class SolarPanelNonLinear
extends Object

Activity written to demonstrate how the scheduler might handle uncontrollable durations. This is a representation of a solar articulation activity For long articulations, the articulation is split into three segments: (1) acceleration leg, (2) coast leg (no accel), (3) deceleration leg. The arrays will accelerate at the max accel up to the max rate, coast for some time at the max rate, and decelerate to zero to complete the turn (where the array has now rotated by the turn angle). This is a trapezoidal profile (since the angular velocity curve is shaped like a trapezoid). For shorter articulations, we may never accelerate long enough to hit the max rate; we just accelerate for a little bit and start decelerating (all at the max accel). This is what we’d call a triangular profile.

Field Summary

Fields

Modifier and Type	Field	Description
double	alpha_max
double	omega_max
double	theta_turn

Constructor Summary

Constructors

Constructor	Description
SolarPanelNonLinear()

Method Summary

Modifier and Type	Method	Description
static double	duration(double theta_turn, double alpha_max, double omega_max)
void	run(Mission mission)

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Details

theta_turn

public double theta_turn

alpha_max

public double alpha_max

omega_max

public double omega_max

Constructor Details

SolarPanelNonLinear

public SolarPanelNonLinear()

Method Details

duration

public static double duration(double theta_turn,
 double alpha_max,
 double omega_max)

run

public void run(Mission mission)