Login and get your AI feedback from Ludwig. Login and get your AI feedback from Ludwig.
Login and get your AI feedback from Ludwig.
Such calculations are not easy, because it is impossible to predict exactly how a tumbling spacecraft will break up as it re-enters.
We discuss an angular momentum control of a tumbling spacecraft.
This will ensure the tumbling spacecraft does not interfere with other satellite communications.
Given this solution, a constant state filter is proposed for inertial characteristics estimation and attitude prediction of tumbling spacecraft.
It is concerned with servicing to a tumbling non-cooperative target spacecraft in arbitrary orbit subjected to external disturbances.
One dire possibility is that the spacecraft is tumbling, which would cause the batteries to discharge since the solar panels no longer point toward the sun.
How the spacecraft tumbles through the atmosphere has an influence on how it breaks up.
Awesome tool! I started using it one year ago and I never had to look for another app
Ha Thuy Vy
MA of Applied Linguistic, Maquarie University, Australia