Abstract

This paper proposes a warning threshold calculation method for instantaneous collision probability in a spacecraft rendezvous mission. By introducing missing alarm probability, the warning threshold is determined as a function of the propagated trajectory uncertainty and a semianalytical calculation model is presented. The simulation results show that the proposed method makes good use of trajectory uncertainty information and provides a reasonable and accurate method for evaluating the safety of a rendezvous trajectory with uncertainty.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call