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White Paper: Multiple Model Propagation Of High Area-To-Mass (HAMR) Objects Using An Encke Type Correction Algorithm
This paper examines performance of the original algorithm for a different orbit regime, and for a wider range of object shapes and attitude motions.
Read MoreImportant Concepts in the Development of the STK Object Model
- May 17, 2017
- Ismir Tufek
- Tech Tip
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STK Engine on Windows and Linux: the NoGraphics Mode Feature
- Dec 22, 2016
- Sylvain Dupont
- Tech Tip
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White Paper: Covariance Realism
Covariance information from orbit determination is being relied upon for space operations now more than ever.
Read MoreWhite Paper: Determination of close approaches based on ellipsoidal threat volumes
A method for computing close approach events for space objects having ellipsoidal threat volumes is presented.
Read MoreWhite Paper: Effect Of Coordinate Selection On Orbit Determination
This paper shows the effects of coordinate selection on orbit determination
Read MoreWhite Paper: Global Atmospheric Density Estimation Using A Sequential Filter/Smoother
This paper shows the global atmospheric density estimation using a sequential filter/smoother
Read MoreSTK Components
Build custom applications on a foundation of STK’s algorithms and capabilities.
Read MoreWhite Paper: Investigating Orbital Debris Events Using Numerical Methods With Full Force Model Orbit Propagation
This paper describes the investigation of orbital debris events using numerical methods with full force model orbit propagation.
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