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Starling Formation-Flying Optical Experiment: Initial Operations and Flight ResultsThis paper presents initial flight results for angles-only navigation of a swarm of small spacecraft, conducted during the Starling Formation-Flying Optical Experiment (StarFOX). StarFOX is one of four experiments aboard the NASA Starling mission, which consists of four CubeSats launched in July 2023. Angles-only methods apply inter-satellite bearing angles obtained by on-board cameras for navigation, increasing satellite autonomy and enabling new mission concepts. Nevertheless, prior flight demonstrations have only featured one observer and target and have relied upon a-priori target orbit knowledge for initialization, translational maneuvers to resolve target range, and external absolute orbit updates to maintain convergence. StarFOX overcomes these limitations by applying the angles-only Absolute and Relative Trajectory Measurement System (ARTMS), which integrates three novel algorithms. Image Processing detects and tracks multiple targets in images, using multi-hypothesis methods and domain-specific kinematic modeling, and computes target bearing angles. Batch Orbit Determination computes initial swarm orbit estimates from bearing angle batches, via iterative batch least squares and sampling of the weakly observable target range. Sequential Orbit Determination leverages an adaptive, efficient unscented Kalman filter with nonlinear models to refine swarm state estimates over time. Multi-observer measurements shared over an intersatellite link are seamlessly fused to enable robust absolute and relative orbit determination. Initial StarFOX experiments are the first demonstrations of autonomous angles-only navigation for a satellite swarm, including multi-target and multi-observer relative navigation; autonomous initialization of navigation for unknown targets; and simultaneous absolute and relative orbit determination. Relative navigation accuracy of 1% (single observer) and 0.2% (multi-observer) of the inter-satellite range
is achieved under challenging measurement conditions. Results demonstrate promising performance with regards to ongoing StarFOX campaigns and the application of angles-only navigation to future distributed missions.
Document ID
20240007230
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Justin Kruger
(Stanford University Stanford, United States)
Simone D'Amico
(Stanford University Stanford, United States)
Soon S Hwang
(Ames Research Center Mountain View, United States)
Date Acquired
June 5, 2024
Publication Date
June 10, 2024
Publication Information
Publication: Proceedings of the 38th Annual Small Satellite Conference
Publisher: Small Satellite Conference
Volume: SSC24
URL: https://digitalcommons.usu.edu/smallsat/
Subject Category
Space Sciences (General)
Space Communications, Spacecraft Communications, Command and Tracking
Spacecraft Design, Testing and Performance
Report/Patent Number
SSC24-XI-01
Meeting Information
Meeting: 38th Annual Small Satellite Conference
Location: Logan, UT
Country: US
Start Date: August 3, 2024
End Date: August 8, 2024
Sponsors: Utah State University
Funding Number(s)
CONTRACT_GRANT: 80NSSC18M0058
CONTRACT_GRANT: 80ARC020D0010
CONTRACT_GRANT: 80ARC021D0001
OTHER: FA9550-21-1-0414
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Relative Navigation
Vision based Navigation
Relative Orbit Estimation
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