Dual quaternion kalman filters for spacecraft relative navigation

Yigal Zivan, Daniel Choukrouny

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

6 Scopus citations

Abstract

This work presents two novel additive dual quaternion Kalman fllters for position, attitude and sensor biases estimation in a low Earth orbit two-spacecraft relative navigation problem. The spacecraft are assumed to be equipped with sensing suites suitable for close proximity operations, providing biased angular and linear velocities and inter-satellite Line-Of-Sight vision-based observations. Extensive numerical simulations are performed for a typical proximity operation scenario and the fllters’ performances are compared with three state-of-art other algorithms.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Edition210039
ISBN (Print)9781624105265
DOIs
StatePublished - 7 Jan 2018
EventAIAA Guidance, Navigation, and Control Conference, 2018 - Kissimmee, United States
Duration: 8 Jan 201812 Jan 2018

Publication series

NameAIAA Guidance, Navigation, and Control Conference, 2018
Number210039

Conference

ConferenceAIAA Guidance, Navigation, and Control Conference, 2018
Country/TerritoryUnited States
CityKissimmee
Period8/01/1812/01/18

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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