SIMULATOR USER INTERFACE Sample Clauses

SIMULATOR USER INTERFACE. The simulator user interface is implemented on the real-time simulation computer and presents the simulator operator with an easy-to-use menu and icon-based graphical user interface. All of the simulator functionality and controls are accessible through the menus. In addition, some commonly used functions are available on a button bar. This interface allows the operator to configure, monitor, and control the DSS and initiate various simulator failures. The basic features and capabilities of the user interface includes but is not limited to: 1. Management, setup, editing and saving of multiple database sets 2. Display of spacecraft commands and telemetry 3. Commanding via single commands, time-tag commands, or commands files 4. Initiation of spacecraft anomalies and failures from a pick list 5. A variety of display pages, including: a. Raw and some formatted telemetry as engineering units b. Non-telemetered simulation variables (such as “true” yaw) c. Orbit state information d. Event log display e. A three-dimensional graphical display showing the relative angles of the spacecraft, the Sun, the Moon, and Earth 6. Definition of new spacecraft data display screens 7. Selection and display of a set of global variables in real time 8. Display of spacecraft telemetry data and other selected non-telemetry data in real time (while the simulation is running) in a strip-chart form 9. Capability to “fast forward” the orbit to a user-specified time or until the first occurrence that a specified Parameter Identification (PID) is equal to a user specified hex value. The “fast forward” only maintains the attitude state, it is not propagated 10. Display of more than one page at a time 11. Displays that can be printed to a network (or local) printer Figure 1-1 shows some of the core user interface functionality. In the upper left corner is the simulator main menu from which the user will control the simulation. Also shown are the commanding window (upper right) for spacecraft commands from the user interface, the telemetry PID display (lower right), which displays detailed information of any PID, a simplistic three-dimensional display (middle left), the status/event logger (lower left), and a user-definable display with internal variables and telemetry PIDs (lower middle). Figure 1-1. DSS User Interface
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