AppliedDeltaVDPT |
Compute the applied delta-v from the applied force. |
ComputeDeltaV |
Takes the 3-axis force in [kg*m/s/s] and computes the delta-v in [m/s]. |
ComputeDistance |
Computes the distance of each spacecraft from the center, given the |
DerivationTemplate |
The template for new derivation functions. |
Difference |
Differences two vectors. |
DifferenceMagnitude |
Compute the magnitude of the difference between vectors. |
ECI2HillsDFF |
Transform ECI pos & vel to Hills pos & vel. |
MagDPT |
Compute the Magnitude of a vector of data in the PlottingTool. |
RV2ElDPT |
Transform ECI position and velocity into orbital elements. |
RotateECI2Hills |
Transform ECI frame coordinates to Hills frame |
SMADiffDPT |
Compute the semi-major axis difference between each spacecraft and its reference |
TransformECI2Hills |
A Plotting Tool derivation function for transforming ECI coordinates to Hills frame |
x2r |
Takes a 6 state input and returns the first 3 states (position). |
x2v |
Takes a 6 state input and returns the 3 state output (velocity). |
FormatUnderscore |
Replaces all underscores in strings with '\\_' so that the underscore is not |
GetSimData |
Get the data from an ObjectAgent simulation |
InitializeAxes |
Initialize the axes for an animation. |
PTVersion |
Output the version string. |
PlotCone |
Creates a cone with angular width 2*theta about the vector u. |
PlotEngine |
Create figures with automatically labeled and organized plots. |
PlotVector |
Plots a set of 2-D or 3-D vectors. |
PlottingToolStruct |
Save 3D trajectories in the PlottingTool format. |
ReadOASimulationFile |
Read in output text file generated by OA dynamics simulation |
ReadOutputFile |
Read in simulation output text file for use with the PlottingTool. |