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STK/Astrogator

STK/Astrogator STK/Astrogator STK/Astrogator is a specialized analysis module for interactive orbit maneuver and spacecraft trajectory design. It supports an unlimited series of events for modeling and targeting a spacecraft’s trajectory, including impulsive and finite burns and high-fidelity orbit propagation. Event triggers allow users to focus on overall mission needs without having to perform off-line calculations to set up the problem. It offers tremendous flexibility through the use of customized force models, engine models, and spacecraft attitude, along with the ability to solve for and optimize solutions.

STK/Astrogator provides analysis of the entire trajectory, which can be used as the foundation for an overall STK system analysis, including sensor coverage and constrained station visibility opportunities for quick, easy analysis of the whole picture. Mission segments can be stored with STK scenarios and later edited as the mission proceeds. During flight operations, a user can refine maneuver plans with flight-generated data—such as engine-calibration parameters and actual initial orbits—to produce thruster firing and timing data for command generation. Used with STK Professional Edition, STK/Astrogator generates dramatic 3-D representations of space missions ranging from low-Earth orbit (LEO) to interplanetary trajectories.

  • Highlights

    • Leverages all STK functionality
    • Visualization with STK Professional Edition
    • Finite and impulsive burn modeling
    • Targeted maneuver sequences
    • Fuel-usage calculations
    • Sophisticated event detection capability
    • Deep space mission design and analysis
    • Industry-standard atmospheric density models—exponential, Harris-Priester, Jacchia 1971, Jacchia-Roberts, Cira 72, MSIS, US Standard
    • Custom central bodies and force models
    • High precision numerical integrators—Runge-Kutta-Fehlberg, Runge-Kutta-Verner, Burlisch-Stoer, Gauss-Jackson
    • Parameter optimization

  • Key Features

  • STK/Astrogator

    Mission control sequence

    A Mission Control Sequence (MCS) tree displays the sequencing and structure of the mission and facilitates the editing of mission segments. The MCS is a graphical programming language, using mission segments that dictate how STK/Astrogator will build the spacecraft trajectory. Individual mission segments are added as the building blocks of the mission, and can be keyed to temporal, orbital or system events, including constrained inter-visibility opportunities with other satellites or ground stations.

    Targeter

    STK/Astrogator calculates maneuver characteristics necessary to meet mission requirements by using a mission segment called a target sequence. Within a target sequence, a differential corrector algorithm adjusts user-defined control variables to satisfy user-defined constraints. Nested target sequences can meet the most demanding trajectory designs by solving for segments of the overall trajectory while iterating on the complete solution. Automatic sequences can be designed to ensure that specific mission control steps are applied every time user-defined conditions occur, an ideal feature for station-keeping, orbit-raising, and orbit-lowering.

    Built-in trajectory optimization

    STK/Astrogator provides powerful optimization capability at the segment level via the target sequence. This optimization profile of a targeter allows for coarse->fine->optimized targeting. The ability to optimize maneuvers is critical to successfully targeting subsequent portions of the mission via the MCS.

    High-fidelity orbit propagation

    STK/Astrogator's flight-proven algorithms include force models for third-body effects, solar radiation pressure, atmospheric drag, geopotential models, thermal pressure and albedo and solid and ocean tides, as well as the use of JPL planetary ephemeris data for accurate coordinate transformations including precession, nutation and pole wander. Users can choose from a broad set of numerical integrators.

    Component technology

    STK/Astrogator includes a Component Browser and Editor for selecting and customize engine models, force models, propagators, coordinate systems, central bodies, atmospheric models and other elements of a space mission analysis scenario. These elements can then be used or adapted in any STK/Astrogator scenario. STK's Vector Geometry Tool builds upon the standard vectors, coordinate systems, state variables and angles to create unique components for use in building mission control sequences. You can use STK/Astrogator components as target and stop values, and as the basis for reports.

    Scripting/Plugin interface

    STK/Astrogator is a fully customizable astrodynamics software platform that can control or be controlled by outside scripts and plugins. Choose from numerous programming environments (Perl, MATLAB, Excel, VBS, Java, .NET) and write external scripts to control numerical integration, engine models, spacecraft attitude or targeter search methods. You can also apply custom logic from within the MCS via a simple scripting interface in the GUI. This capability allows users to easily solve much more complicated trajectory problems such as tying multiple maneuvers together or applying a solved-for attitude or a percentage of a required total delta-v for a given maneuver.

    Multiple views of space missions

    Using STK's multiple map window capability, STK/Astrogator lets you view a mission or a mission segment from as many perspectives and distances as your screen allows. In addition, when used with STK Professional Edition, you can display multiple 3-D views of the mission. Spacecraft trajectories can be viewed in inertial, fixed or any user-defined frame, and monitored during successive calculation iterations of the targeter in 3-D for critical insight into the targeting solution.

    Closed-loop maneuver control

    Model closed-loop propulsion systems and maneuver control laws to analyze missions which include near-field rendezvous, proximity operations, station-keeping, planetary landing and formation flying. Analyze fuel requirements, thruster duty cycles and control-law stability and robustness, among others.

    Formation flying

    STK/Astrogator models multiple spacecraft flying in formation, thus permitting users to analyze and calculate complex maneuvers that support formation-flying activities such as imaging, satellite maintenance missions, gravity field determination and constellation maintenance. To complement numerical results, visualize complex trajectories in a vehicle-relative coordinate frame with STK Professional Edition.

    Reports and graphs

    STK/Astrogator generates a variety of reports and graphs, including reports concerning the numerous elements of a trajectory at the conclusion of the mission or at any phase during the mission. STK/Astrogator also reports on the corrections introduced by a target sequence and the extent of its success in achieving the assigned goals. Building upon the STK/Astrogator component technology, all kinds of data can be output in customizable fashion.

AGI Support

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Supported OS and Hardware Requirements

Supported Operating Systems
  • Windows
  • XP Professional
  • Server 2003, 2008
  • Vista
  • Windows 7
  • Linux (TBA)
Minimum Hardware Requirements
  • 1.4 GHz Core Duo Processor
  • 2 GB RAM, 1 GB Disk Space for Installation
  • Dedicated Storage for Data, based on your needs
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