High Frequency, High Accuracy Pointing onboard Nanosats using Neuromorphic Event Sensing and Piezoelectric Actuation
Yasir Latif, Peter Anastasiou, Yonhon Ng, Zebb Prime, Tien-Fu Lu,, Matthew Tetlow, Robert Mahony, Tat-Jun Chin

TL;DR
This paper presents a novel nanosatellite payload combining neuromorphic event sensing and piezoelectric actuation to achieve high-frequency, high-accuracy pointing stabilization, significantly improving current nanosat attitude control capabilities.
Contribution
The work introduces a neuromorphic event sensor paired with piezoelectric actuation for stable, high-frequency pointing in nanosats, demonstrating a new approach for space attitude control.
Findings
Achieved 1-5 arcseconds pointing accuracy
Operated at up to 50Hz frequency
Used commercial-off-the-shelf components
Abstract
As satellites become smaller, the ability to maintain stable pointing decreases as external forces acting on the satellite come into play. At the same time, reaction wheels used in the attitude determination and control system (ADCS) introduce high frequency jitter which can disrupt pointing stability. For space domain awareness (SDA) tasks that track objects tens of thousands of kilometres away, the pointing accuracy offered by current nanosats, typically in the range of 10 to 100 arcseconds, is not sufficient. In this work, we develop a novel payload that utilises a neuromorphic event sensor (for high frequency and highly accurate relative attitude estimation) paired in a closed loop with a piezoelectric stage (for active attitude corrections) to provide highly stable sensor-specific pointing. Event sensors are especially suited for space applications due to their desirable…
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Taxonomy
TopicsInertial Sensor and Navigation · Spacecraft Design and Technology · Space Satellite Systems and Control
