Description
Engine properties for a Optimal Finite Maneuver.
Public Methods
 ExportNodes | Exports the current set of collocation nodes to a file. |
| RunSeed | Run seed. |
Public Properties
 DiscretizationStrategy | Discretization Strategy. |
| EnableUnitVectorControls | Enable unit vector for thrust direction. |
| ExportFormat | Format for exporting collocation control variables. |
| FinalBoundaryConditions | Final Boundary Conditions. |
| HaltMCSWhenNoConvergence | Halt MCS and discard result if optimization is unsuccessful. |
| InitialBoundaryConditions | Initial Boundary Conditions. |
| InitialGuessFileName | File containing ephemeris for nodes that serve as an initial guess. |
| InitialGuessInterpolationMethod | Guess interpolation method. |
| LogFileName | Log file name for optimal finite maneuver. |
| NodeStatusMessage | A message that indicates what nodes are currently held by the segment. |
| NumberOfNodes | Number of nodes to discretize collocation problem into. |
| PathBoundaryConditions | Path Boundary Conditions. |
| PressureMode | The pressure mode. |
| RunMode | Run mode. |
| ScalingOptions | Scaling Options. |
| SeedMethod | Initial seed method. |
| ShouldReinitializeSTMAtStartOfSegmentPropagation | If this segment is propagating the state transition matrix, reset it to the identity matrix at the start of the segment. |
| SNOPTOptimizer | SNOPT Optimizer Options. |
| SteeringNodes | The list of steering nodes. |
| ThrustAxes | Label reflecting coordinate axes for the thrust vector |
| ThrustEfficiency | The fraction of ideal thrust applied. Any number above zero is valid, with typical values around 0.98 to 1.02. Dimensionless. |
| ThrustEfficiencyMode | Thrust - the calculations that are effected by the thrust efficiency value. |
| WorkingVariables | Working Variables. |
Interfaces
| Implemented Interface |
|---|
| IAgVAManeuver |