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Simulating Attacks from North Korea

  • Sep 12, 2017
  • Jeff Baxter
  • Article

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White Paper: Least Squares GEO Initial Orbit Determination

  • PDF

This paper describes a new fast-running algorithm to perform refined orbit determination for any spacecraft in GEO (geosynchronous earth orbit).

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Indian ASAT Forensics - April 9, 2019 Update

  • Tom Johnson, Dan Oltrogge, Dr. T.S. Kelso
  • Video

Analysis and debris simulation of India's direct ascent ASAT weapons test on 3-27-2019.

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EOIR

Model electro-optical and infrared sensor performance.

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Space Traffic Management - Spacecast 21

  • Jim Cooper
  • Video

Jim Cooper discusses Space Traffic Management (STM) challenges including space debris tracking and upcoming large constellations of satellites.

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STK 11.7: STK Engine on Linux and MTK

  • Nov 4, 2019
  • Nathan Matz
  • Blog Post

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White Paper: Multiple Model Propagation Of High Area-To-Mass (HAMR) Objects Using An Encke Type Correction Algorithm

  • PDF

This paper examines performance of the original algorithm for a different orbit regime, and for a wider range of object shapes and attitude motions.

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ODTK SSA

Reverse engineer spacecraft maneuvers, and examine and correct observation association problems.

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White Paper: Covariance Realism

  • PDF

Covariance information from orbit determination is being relied upon for space operations now more than ever.

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White Paper: Determination of close approaches based on ellipsoidal threat volumes

  • PDF

A method for computing close approach events for space objects having ellipsoidal threat volumes is presented.

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White Paper: Effect Of Coordinate Selection On Orbit Determination

  • PDF

This paper shows the effects of coordinate selection on orbit determination

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White Paper: Global Atmospheric Density Estimation Using A Sequential Filter/Smoother

  • PDF

This paper shows the global atmospheric density estimation using a sequential filter/smoother

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White Paper: Investigating Orbital Debris Events Using Numerical Methods With Full Force Model Orbit Propagation

  • PDF

This paper describes the investigation of orbital debris events using numerical methods with full force model orbit propagation.

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STK Supports Missile Test Analysis

  • PDF

STK helps the System Test and Evaluation Planning Analysis Lab (STEPAL), which serves the Missile Defense Agency (MDA)

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