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Connect digital engineering to the mission level with STK 12
- Apr 29, 2020
- Washington Wedderburn
- Blog Post
Take your mission development to the next level with the newest STK version, STK 12.
Read MoreWhite Paper: Effects of Eclipse Boundary Crossings on the Numerical Integration of Orbit Trajectories
This paper shows the effects of eclipse boundary crossings on the numerical integration of orbit trajectories
Read MoreWhite Paper: Ephemeris Requirements For Space Situational Awareness
This paper describes the ephemeris requirements for Space Situational Awareness (SSA).
Read MoreWhite Paper: Determination of close approaches for Earth fixed launch trajectories
This paper shows how to determine close approaches for Earth fixed launch trajectories
Read MoreImproving Analysis with the Navigation Analysis Plugin
- Dec 12, 2016
- Richard DeYoung
- Tech Tip
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White Paper: A Preliminary Analysis of State Vector Prediction Accuracy
This paper shows numerical results for propagating satellite state vectors against known POE’s and against precise ephemerides
Read MoreWhite Paper: Determination of close approaches for constellations of satellites
This paper shows how to determine close approaches for constellations of satellites.
Read MoreWhite Paper: Getting To Know Our Space Population From The Public Catalog
Our space population continues to increase as satellites are launched and debris producing catastrophic events occur.
Read MoreWhite Paper: Integration Of Orbit Trajectories In The Presence Of Multiple Full Gravitational Fields
- Dr. Vince Coppola
Describes the integration of trajectories in the presence of multiple full gravitational fields
Read MoreWhite Paper: Mitigation of the Effects of Eclipse Boundary Crossings
This paper describes the mitigation of the effects of eclipse boundary crossings
Read MoreWhite Paper: Determination Of Orbit Cross-Tag Events And Maneuvers With Orbit Detective
This paper shows how to determine the orbits of cross tag events and maneuvers with orbit detective.
Read MoreWhite Paper: Efficient Numerical Integration of Coupled Orbit and Attitude Trajectories
This paper shows the efficient numerical integration of coupled orbit and attitude trajectories using and Encke Type correction algorithm
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