Visualizing Data Manipulating the 3D Orbit View Configuring the Ground Track Plot Creating a 2D Plot IV. Reporting Data Reporting Data During a Propagation Span Reporting Data at a Specific Mission Event Creating a CCSDS Ephemeris File Creating an SPK Ephemeris File 7. Propagating a Spacecraft Configuring the Force Model Configuring the Force Model: Mars Propagating for a Duration Propagating to an Orbit Condition 6. Configuring a Spacecraft Setting the Initial Epoch Configuring the Orbit Configuring Physical Properties Configuring the Attitude (Fixed) Configuring the Attitude (Spinner) 5. Simulating an Orbit Objective and Overview Configure the Spacecraft Rename the Spacecraft Set the Spacecraft Epoch Set the Keplerian Orbital Elements Configure the Propagator Rename the Propagator Configure the Force Model Configuring the Orbit View Plot Configure the Propagate Command Run and Analyze the Results III. Getting Started Installation Starting and Quitting GMAT Starting a GMAT Session Quitting a GMAT Session Running the GMAT Demos User Interfaces Overview GUI Overview Script Interface Overview GUI/Script Interface Interactions and Rules Data and Configuration File Structure Configuring GMAT Data Files Configuring the MATLAB Interface Other Resources II. Introduction to GMAT Licensing Platform Support User Interfaces Development Status Contributors 2. Table of Contents Preface Introduction Creating Your First Mission Common Tasks Tutorials Reference Guide Typographical Conventions I.
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