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STK/EOIR - COTS modeling and simulation software for EO/IR sensors

STK/EOIR STK-EOIR

STK/EOIR models detection, tracking and imaging performance of electro-optical and infrared sensors for

  • Space Situational Awareness
  • Missile Defense
  • Earth Remote Sensing

STK/EOIR lets anyone who understands system-level sensor specifications improve their STK mission model with radiometric performance prediction. This is a unique alternative to complex stand-alone sensor simulations.

STK/EOIR is developed by Space Dynamics Laboratory (SDL), an AGI business partner and industry leader in electro-optical and infrared sensor systems. For over 50 years SDL has designed, fabricated, tested, and deployed sensors for customers including NASA, the U.S. Air Force and the U.S. Missile Defense Agency.

Schedule a technical demonstration:
Virtual or on-site demo of STK/EOIR with an AGI technical expert
Click here to request resources from the AGI webinar:
EO/IR Sensor Analysis in STK
  • Highlights

    • Physics-based radiometric sensor model
    • Ultraviolet, visible and infrared bands (0.28 - 28 microns)
    • Example outputs:
      • Target signal-to-noise ratio (SNR)
      • Sensor output image synchronized to the STK 3D animation window
      • ASCII sensor pixel data file for processing in MATLAB, MathCAD, Excel
    • Low complexity for rapid analysis and accessibility by non-experts
    • Integrated sensor and mission analysis to model important system interactions
    • Anchored against operational missile defense sensor measurements
    • STK/EOIR Brochure
  • Key Features

  • Target modeling

    Model optical and thermal properties of satellites, space debris and missiles by specifying shape, dimensions, surface material and surface temperature. Missile targets can be multi-staged with independent stage properties and solid black body plume model (temperature and emissivity).

    Accurate star field

    Leverage STK's database of over two million high quality star records from the Hipparcos and Tycho II catalogs to model precise position and spectral irradiance based on apparent motion, temperature and magnitude.

    Celestial bodies

    Include thermal and optical properties of the Earth, Moon, Sun and planets. Thermal models include diurnal, latitudinal, and seasonal variations. Optical surface properties maps are included for the Earth, Moon and Mars at 0.93 km, 2.5 km and 0.47 km resolutions respectively. The Earth includes an atmospheric model with four aersol settings.

    Sensor specification

    Use just a small set of common system level specifications to fully characterize the performance of a proposed or operational sensor design. This speeds analysis and makes STK/EOIR accessible to sensor designers and general systems engineers alike.

    • Angular field of view extents
    • Focal plane height and width in pixels
    • Number of detection bands
    • Lower and upper band edges
    • Band integration time, sensitivity (NEI, NER) and dynamic range (SEI, SER)
    • Effective focal length
    • Entrance pupil diameter
    • Diffraction wavelength
    • Longitudinal defocus
    • Image quality (zero, negligible, mild or moderate aberrations)
    • Line of sight jitter

    Sensor performance

    Report radiometric performance for point sources and extended objects through STK reports, graphs and dynamic displays. Metrics include target radiance/irradiance, background radiance/irradiance, scene photon signal-to-noise ratio (SNR), noise equivalent irradiance (NEI) and noise equivalent radiance (NER).

    Sensor output images

    See what the sensor would see via a dynamic sensor output image display. Improve interpretation and analysis by comparing against synchronized views in the STK 3-D display and a synthetic sensor input scene window. Export sensor output images as ASCII files for use in image processing algorithms modeled in MATLAB, MathCAD or Excel.

    Multi-sensor architecture analysis

    Model mission architectures with up to six independently specified and steered sensors distributed across any mix of satellite, aircraft, ship or ground platforms.

AGI Support

Hours

  • Monday - Thursday: 6 a.m. - 10 p.m. ET
  • Friday: 6 a.m. - 8 p.m. ET

Phone

  • 1.800.924.7244
  • 1.610.981.8888

E-mail

Try AGI's Public ADF Server
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  2. Step by Step ADF Tutorial

See the ADF Administrators Guide for specific information about configuring an ADF Server.

Follow instructions below to request a 90 day evaluation license and the ADF Server Installation download link.

AGI Data Federate requires the use of a FlexNET License Server to host your license.

Obtain the Host ID and the Hostname or IP Address:

  • Start All Programs/Accessories/Command Prompt. Right-click to 'Run as administrator'.
  • At the prompt, enter ipconfig /all
  • Under Ethernet adapter Local Area Connection, note:
    • Physical Address (Host id)
    • IPv4 Address (IP Address)
  • Send this to AGI Support (moc.iga@troppus), with the subject line "Request for ADF Licenses."

You will receive an e-mail containing

  1. ADF Server Installation download link
  2. Detailed instructions for installing the License Server.
  3. Users are provided two *.lic files; a server license file installed on the FlexNET License Server and a client license, installed during the AGI Data Federate Server installation.

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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