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Session D3: Space Navigation and Observation

Relative Navigation Methods for a Multi-Agent, On-Orbit Inspection Mission
Mark Mercier and David Curtis, Air Force Institute of Technology
Location: Cypress
Date/Time: Wednesday, Apr. 26, 10:40 a.m.

Abstract—On-orbit inspection is often a necessary prerequisite to satellite operations such as servicing and debris removal. In particular, multiple inspectors collaborating to inspect an unknown object can result in a faster and more comprehensive inspection. The contribution of this research is to provide a reliable, computationally efficient estimate for the position of each agent relative to a target in a multi-agent inspection. First, an overview of the problem dynamics, background, and methods used to build and solve a factor graph-based estimation technique is provided. Through the implementation of a Sliding Window (SW) filter, a factor graph can be applied to long duration scenarios while reducing processing requirements for estimation. An example scenario of three agents attempting to conduct an inspection while susceptible to a Sun exclusion zone that nulls some measurement information is prescribed. Development continues by comparing results for the developed Sliding Window Factor Graph (SWFG) against two extreme SW sizes of interest: an iterative Kalman filter (SW size = 1) and a full factor graph (SW size ? scenario duration). Results reveal the impact of both the Sun exclusion zone and sliding window size on estimation quality and computation time.
Index Terms—Space Technology, Satellite Inspection, Relative Navigation, Multi-Agent.

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