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STAR
Cal STAR — firmware, DAQ server, and engine design
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Static Public Attributes | |
| float | h = Field(..., description="Altitude [m]") |
| float | vz = Field(..., description="Vertical velocity [m/s]") |
| float | theta = Field(default=0.0, description="Tilt angle [rad]") |
| Optional | mass_estimate = Field(default=None, description="Vehicle mass estimate [kg]") |
Navigation state data.
Definition at line 176 of file control.py.
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static |
Definition at line 178 of file control.py.
Referenced by engine.control.robust_ddp.data_models.NavState.__post_init__(), engine.core.injectors.impinging._RingManifold.march(), test_injector_layout.TestChannels.test_channel_flow_area_is_reported_against_the_orifices(), test_injector_layout.TestContouredFace.test_clearances_are_to_the_groove_edges(), test_injector_layout.TestContouredFace.test_each_exit_is_square_on_its_flank(), test_injector_layout.TestContouredFace.test_exits_share_one_recessed_plane(), test_injector_layout.TestContouredFace.test_flat_face_keeps_the_old_geometry(), test_injector_layout.TestContouredFace.test_free_jet_is_measured_along_the_jet(), test_injector_layout.TestContouredFace.test_groove_edges_and_depth(), test_injector_layout.TestChannels.test_passage_runs_its_L_over_d_to_the_channel_floor(), test_injector_layout.TestContouredFace.test_the_jets_meet_where_trigonometry_says(), and engine.control.robust_ddp.data_models.NavState.to_dict().
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static |
Definition at line 181 of file control.py.
Referenced by engine.control.robust_ddp.data_models.NavState.to_dict().
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static |
Definition at line 180 of file control.py.
Referenced by engine.control.robust_ddp.data_models.NavState.to_dict().
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static |
Definition at line 179 of file control.py.
Referenced by engine.control.robust_ddp.data_models.NavState.to_dict().