Styles by Object | Reports | Graphs
Installed Styles: Missile
The following is the list of installed Report and Graph styles for use with the Report Manager. Users may create their own styles to report/graph their desired content using the available data providers.
Reports
| Name | Description |
|---|---|
| Active Constraints | Lists the constraints that are applied when computing the access. |
| Altitude vs Ground Range | The ground range and altitude of the vehicle over time. |
| Attitude Quaternions | The attitude quaternion of the vehicle's body axes computed with respect to the vehicle's central body inertial coordinate system. The quaternion components q1, q2, and q3 are the vector components of the quaternion; q4 is the scalar part. |
| Attitude Schedule | The list of attitude segments describing the attitude for this object. Each segment is valid over its defined interval. |
| Beta Angle | Reports the beta angle (i.e., the signed angle of the apparent vector to the Sun) over time, relative to the orbital plane. The signed angle is positive when the apparent vector is in the direction of the orbit normal. The orbit normal (which is normal to the orbital plane) is parallel to the orbital angular momentum vector, which is defined as the cross-product of the inertial position and velocity vectors. |
| Close Approach | Reports Close Approach tool settings and the list of conjunctions between the object and secondary vehicles that eventually become within a specified minium range threshold, as computed by the Close Approach tool. |
| DeckAccess | Reports the output from the Deck Access tool. The Deck Access tool allows you to compute access to a set of objects, not currently defined within the STK scenario, from a single object within the scenario. |
| DeckAccessCommonName | Reports the output from the Deck Access tool, including the common name if available. The Deck Access tool allows you to compute access to a set of objects, not currently defined within the STK scenario, from a single object within the scenario. |
| Eclipse Times | Generates a listing of all eclipse events. Eclipsing events are start and end of periods of partial lighting (penumbra) and periods of zero lighting (umbra). |
| Ephemeris-IFT | The position and velocity of the object with respect to Earth, as observed from its AlignmentAtEpoch coordinate system, expressed in Cartesian components as a function of time. The AlignmentAtEpoch system is the non-rotating coordinate system (i.e., a constant offset from ICRF) coincident with the Fixed system evaluated at the object's coordinate reference epoch (usually, the initial orbit epoch). Only available for objects whose central body is Earth. |
| Ephemeris-IFT-LLA | The position of the object (expressed in LLA elements), and the velocity of the object (expressed in Cartesian components of the object's central body's Fixed coordinate system) as a function of time. |
| EphemerisChooseAxes | Reports the object's Position and Velocity vectors in a specified reference set of axes. The user chooses the reference axes, which must be defined in the Vector Geometry Tool. |
| Euler Angles | 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, as a function of time. Euler angles use a sequence of three rotations starting from a reference coordinate frame. The rotations are performed in succession: each rotation is relative to the frame resulting from any previous rotations. The 313 sequence uses Z, then the new X, and then finally the newest Z axis. |
| Fixed Acceleration | The acceleration 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. |
| Fixed LLR Position | The ephemeris of the object with respect to the object's central body, as observed from the Fixed coordinate system, expressed in LLR elements as a function of time. |
| Fixed Position Velocity | 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 Acceleration | The acceleration 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. |
| J2000 Position Velocity | 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. |
| LLA Position | The ephemeris of the object, expressed in LLA elements, as a function of time. The coordinate system is the Fixed frame of the object's central body. |
| Launch Window Blackouts | Launch Window tool settings and the launch time intervals where at least one conjunction will occur with a secondary vehicle, if the object were to launch during that interval, as computed by the Launch Window tool. A conjunction occurs if the object would become with the specified minimum range threshold to a secondary vehicle at some later time. |
| Launch Window Clear Intervals | Reports Launch Window tool settings and the launch time intervals where no conjunctions to any secondary vehicle occur, as computed by the Launch Window tool. A conjunction is deemed to occur if the object, having launched during that interval, would become with the specified minimum range threshold to a secondary vehicle at some later time. |
| Lighting Times | A listing of lighting intervals organized into 3 sections: (i) sunlight (full lighting) intervals, (ii) penumbra (partial lighting) intervals, and (iii) umbra (zero lighting) intervals. |
| Model Area | The area of the object's 3D graphics model, as viewed from a given view direction, as computed by the Area Tool. |
| Penumbra | A listing of the penumbra (partial lighting) intervals. |
| Penumbra Start | A listing of the penumbra (partial lighting) start times. |
| Penumbra Stop | A listing of the penumbra (partial lighting) stop times. |
| Re-entry Angle | Reports the altitude and Re-entry Angle (i.e., the angle between the Fixed velocity direction of the object to the local horizontal plane), and their rates as a function of time. |
| Solar AER | The azimuth, elevation, and range of the apparent relative position vector of the Sun over time, with respect to Inertial VVLH axes (ECIVVLH). |
| Solar Intensity | The percent of the solar disc visible over time. |
| Sun | A listing of the sunlight (full lighting) intervals. |
| Sun Start | A listing of the sunlight (full lighting) start times. |
| Sun Stop | A listing of the sunlight (full lighting) stop times. |
| Sun Vector Fixed | 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. |
| Sun Vector J2000 | The apparent relative position of the Sun to the object, expressed in Cartesian components, using the object's central body's J2000 coordinate system, as a function of time. |
| Swath Points | The location of the object's horizon on the central body surface that is to the side of the motion of the object,
reported as left and right horizon points over time. The left horizon point is on the left side of the horizontal component of velocity vector,
where the velocity vector is measured as observed from the object's central body fixed coordinate system.
The horizontal component is that component not along the detic zenith of the object. The right horizon point is on the right side.
For the Ground Elevation Envelope or Vehicle Half Angle Envelope swath types, the left/right swath point may not exist. If it does not, the point being reported at that time uses the Ground Elevation or Vehicle Half Angle swath setting as appropriate. |
| Umbra | A listing of the umbra (zero lighting) intervals. |
| Umbra Start | A listing of the umbra (zero lighting) start times. |
| Umbra Stop | A listing of the umbra (zero lighting) stop times. |
| Yaw Pitch Roll | 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. YPR angles use a sequence of three rotations starting from a reference coordinate frame. Unlike Euler angles, the
rotations are not made about axes defined by an earlier rotation: each rotation is made about the reference system's axes. The 321 sequence uses Z, then Y, and then
finally the X axis. As used in YPR angles, the names yaw, pitch, and roll do not refer to the angles normally used in aviation; the terms yaw, pitch, and roll in aviation refer to 321 Euler angles. |
Graphs
| Name | Type | Description |
|---|---|---|
| Altitude | Time XY | 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 |
| Altitude vs Ground Range | XY | The altitude of the vehicle plotted against the ground range, as a function of time. |
| Beta Angle | Time XY | Plots the beta angle (i.e., the signed angle of the apparent vector to the Sun) over time, relative to the orbital plane. The signed angle is positive when the apparent vector is in the direction of the orbit normal. The orbit normal (which is normal to the orbital plane) is parallel to the orbital angular momentum vector, which is defined as the cross-product of the inertial position and velocity vectors. |
| Close Approach Periods | Interval | An Interval graph of the conjunction time intervals where at least one conjunction occurs with a secondary vehicle, as computed by the Close Approach tool. A conjunction occurs if the object becomes with the specified minimum range threshold to a secondary vehicle at some time. |
| Cumulative Sunlight | Cumulative Pie | A Pie chart showing the total duration of full sunlight within the graph's requested time interval. Gaps in the chart indicate the total duration of penumbra and umbra durations. |
| Eclipse Times | Interval | An Interval graph of the penumbra (partial lighting) and umbra (zero lighting) intervals. |
| Euler Angles | Time XY | 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. Euler angles use a sequence of three rotations starting from a reference coordinate frame. The rotations are performed in succession: each rotation is relative to the frame resulting from any previous rotations. The 313 sequence uses Z, then the new X, and then finally the newest Z axis. |
| Fixed Position Velocity | Time XY | 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 | Time XY | 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. |
| LLA Position | Time XY | The position of the object, expressed in LLA elements, as a function of time. The coordinate system is the Fixed frame of the object's central body. |
| Launch Window Blackouts | Interval | An Interval graph of the launch time intervals where at least one conjunction will occur with a secondary vehicle, if the object were to launch during that interval, as computed by the Launch Window tool. A conjunction occurs if the object would become with the specified minimum range threshold to a secondary vehicle at some later time. |
| Lighting Times | Interval | An Interval graph of the sunlight (full lighting) intervals, penumbra (partial lighting) intervals and umbra (zero lighting) intervals. Each lighting condition's intervals are plotted on separate lines. |
| Model Area | Time XY | 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 | Time XY | 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 | Time XY | 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 | 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 | Time XY | A plot of the percent of the solar disc visible over time. |
| Sun Vector Fixed | Time XY | 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 | 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 | Time XY | 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. YPR angles use a sequence of three rotations starting from a reference coordinate frame. Unlike Euler angles, the
rotations are not made about axes defined by an earlier rotation: each rotation is made about the reference system's axes. The 321 sequence uses Z, then Y, and then
finally the X axis. As used in YPR angles, the names yaw, pitch, and roll do not refer to the angles normally used in aviation; the terms yaw, pitch, and roll in aviation refer to 321 Euler angles. |