The `missile_graphs` module#

Summary#

Functions

`altitude_line_chart()`	Plot the altitude of the object (i.e., magnitude of the relative position vector between the object and its detic subpoint) as a function of time
`beta_angle_line_chart()`	Plot the beta angle (i.e., the signed angle of the apparent vector to the Sun) over time, relative to the orbital plane.
`cumulative_sunlight_cumulative_pie_chart()`	Create a pie chart showing the total duration of full sunlight within the graph’s requested time interval.
`eclipse_times_interval_graph()`	Create an interval graph of the penumbra (partial lighting) and umbra (zero lighting) intervals.
`euler_angles_line_chart()`	Create a plot of the attitude of the vehicle (i.e., the rotation between the vehicle’s body axes and the vehicle’ central body’s inertial frame), expressed using 313 Euler angles, over time.
`fixed_position_velocity_line_chart()`	Plot the position and velocity of the object with respect to the object’s central body, as observed from its central body’s Fixed coordinate system, expressed in Cartesian components as a function of time.
`j2000_position_velocity_line_chart()`	Plot the position and velocity of the object with respect to the object’s central body, as observed from its central body’s J2000 coordinate system, expressed in Cartesian components as a function of time.
`lighting_times_interval_graph()`	Create an interval graph of the sunlight (full lighting) intervals, penumbra (partial lighting) intervals and umbra (zero lighting) intervals.
`lla_position_line_chart()`	Plot the position of the object, expressed in LLA elements, as a function of time.
`model_area_line_chart()`	Create a plot of the area of the object’s 3D graphics model over time, as viewed from a given view direction, as computed by the Area Tool.
`re_entry_angle_line_chart()`	Create a plot of the altitude and Re-entry Angle (i.e., the angle between the Fixed velocity direction of the object to the local horizontal plane), over time.
`solar_aer_line_chart()`	Create a plot of the azimuth, elevation, and range over time, describing the apparent relative position vector of the Sun with respect to Inertial VVLH axes (ECIVVLH).
`solar_az_el_polar_center_0_graph()`	Create a polar plot with elevation as radius and azimuth as angle theta over time, describing the apparent relative position vector of the Sun with respect to Inertial VVLH axes (ECIVVLH).
`solar_intensity_line_chart()`	Create a plot of the percent of the solar disc visible over time.
`sun_vector_fixed_line_chart()`	Create a plot of the apparent relative position of the Sun to the object, expressed in Cartesian components, using the object’s central body’s Fixed coordinate system, as a function of time.
`sunlight_intervals_interval_pie_chart()`	Create a pie chart showing each interval of full sunlight within the graph’s requested time interval, separated by gaps indicating the intervals of penumbra/umbra lighting condition before and after each sunlight interval.
`yaw_pitch_roll_line_chart()`	Create a plot of the attitude of the vehicle (i.e., the rotation between the vehicle’s body axes and the vehicle’ central body’s inertial frame), expressed using 321 YPR angles, as a function of time.

Description#

Provides graphs for Missile objects.