no code implementations • 29 Apr 2022 • Erdem Turan, Stefano Speretta, Eberhard Gill
This work is based on the Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON) method which provides an autonomous navigation solution solely using satellite-to-satellite measurements, such as range and/or range-rate, to estimate absolute spacecraft states when at least one of the involved spacecraft has an orbit with a unique size, shape, and orientation.
no code implementations • 29 Apr 2022 • Erdem Turan, Stefano Speretta, Eberhard Gill
This study aims at providing a detailed performance analysis of crosslink radiometric measurements based on autonomous orbit determination for cislunar small satellite formations considering the effects of measurement type, measurement accuracy, bias, formation geometry, and network topology.