Converts position and velocity to Keplerian elements.
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#include <rv_to_kepler.h>
Inherits dsim_model.
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| rv_to_kepler (dsim_model_setup *setup) |
| | Constructor.
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| ~rv_to_kepler () |
| | Destructor.
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void | initialize_data () |
| | Initialize outlets and output variables.
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void | initialization_complete () |
| | Finish initialization.
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void | initialize_timestep () |
| | Computation done prior to numerical integration.
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dsim_variable | position_dsim |
| | Spacecraft position matrix, from parent.
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dsim_variable | velocity_dsim |
| | Spacecraft velocity matrix, from parent.
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dsim_variable | muBody_dsim |
| | Planet gravitational constant matrix outlet.
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dsim_variable | observer_dsim |
| | Reference center outlet.
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dsim_variable | planetIndex_dsim |
| | SPICE planet index outlet.
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dsim_variable | keplerian_elements_dsim |
| | Keplerian elements output.
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Converts position and velocity to Keplerian elements.
Computes Keplerian elements given position and velocity vectors.
This module computes Keplerian Orbital elements given the position and velocity of the parent.
The documentation for this class was generated from the following files:
- rv_to_kepler.h
- rv_to_kepler.cc
