Digital Commons Network^™

Lightweight Open Source On-Spacecraft Machine Learning With Mlpack And F Prime, Ryan R. Curtin, Scott M. Gilliland, Sterling L. Peet

Small Satellite Conference

Onboard machine learning is an increasingly important topic in spaceflight systems, as machine learning and AI models are increasingly used for data processing, anomaly detection, attitude control systems, and other predictive applications. However, successfully deploying a machine learning model in a spaceflight computing environment is fraught with difficulty, as spaceflight computing environments are low-resource, but typical machine learning software solutions are implemented in languages like Python, which require an interpreter and other heavyweight dependencies. It is therefore virtually mandatory for any on-spacecraft machine learning to be written with lightweight toolkits that minimize dependencies and resource usage.

We demonstrate a solution …

Scaling Up Monolithic Optics Capabilities: 25cm Aperture And Beyond, Cohl Houldin Hatala, Jordan Smilo, Wim De Vries, Brian Bauman, Christian Tolfa, John Cortes, Paul Rosso, Aaron Godfrey, Darrell Carter, Michael Wong, Seth Cornman, Josephine Smith, John Ganino, Ben Bahney

Small Satellite Conference

The 25 cm “V10” Monolithic Optical Payload has been developed through study phase design into a fully qualified system ready for on-orbit demonstration. This extends Lawrence Livermore National Laboratory’s monolithic telescope technology toward a rapidly fieldable, high performance space imaging system for small and medium spacecraft buses. Centered on the V10 monolithic Cassegrain optic in fused silica, the payload provides highly robust, diffraction limited performance with inherently maintained mirror alignment, eliminating complex on orbit alignment procedures and significantly reducing mechanical risk. The V10 optic is paired with a heritage focus mechanism and a panchromatic commercial off the shelf CMOS detectors, …

Payload Operation Using On-Board Vision Language Model, Meirav Nevo, Oshri Fatkiev, Guy Zaidman, Doron Shterman

Small Satellite Conference

The rapid maturation of multimodal vision-language models (VLMs) has significantly expanded artificial intelligence applications at the edge, including spaceborne systems. In this work, we present one of the first demonstrations of deploying a compact vision-language model directly on a very-high-resolution Earth-observation satellite payload processor, enabling autonomous on-orbit scene understanding and near real-time decision-making. This represents a paradigm shift in satellite operations, moving from ground-centric processing toward intelligent, self-directed spacecraft. 

Conventional Earth-observation missions rely on ground-based image processing and interpretation, introducing latency, downlink bandwidth constraints, and limited operational responsiveness. By embedding a VLM on board the satellite, visual reasoning can be …

A Miniaturized, High Geometric Factor, Electrostatic Analyzer For Fast Plasma Measurements, Dhiren Kataria, Justyna M. Sokol, Jianliang Lin, Camden Ertley, Jonathan Gasser, Guy Grubbs, Kwang-Joo Hwang, Michael Starkey

Small Satellite Conference

With advances in machining techniques that can manufacture high aspect ratio structures at high accuracy, cylindrical geometry electrostatic analyzers present a versatile alternative to spherical designs. We report on the development of the 3D Cylindircal And Tiny Spectrometer (3D-CATS), a novel space plasma analyzer that performs instantaneous 3D (multiple energy, azimuth and elevation angles) measurements, providing differential energy, wide field of view particle imaging in a compact, low-SWaP (size, weight and power) package.

The baseline analyzer design consists of a nest of 8 cylindrical analyzers, providing measurements of incoming particle energy distributions over an energy range of 10 eV to …

Uncertainty Quantification And Platform Scattering For The Cimr Reflector Antenna, Tonny Rubaek, Pasquale Giuseppe Nicolaci, Cecilia Cappellin

Small Satellite Conference

The Copernicus Microwave Imaging Radiometer (CIMR) employs a 7.1 m conical scanning mesh reflector antenna rotating at 7.8 rpm that operates from L to Ka band. Demanding radiometric accuracies and sensitivities at few tenths of a Kelvin at high spatial resolution are targeted for the instrument. These require a high accuracy in the characterization and modelling of the antenna pattern over 4π, considering any nearby scattering structure, and/or any potential multipath due to the antenna installation on the S/C, as well as the quantification of the uncertainty on the beam efficiency (BE) arising (from possible in-orbit random variations in the …

Hyti-2: Advancing Hyperspectral Thermal Imaging Into The Era Of Space-Based Edge Processing, Miguel Nunes, Yosef Onodera, Trevor Sorensen, Robert Wright, Paul Lucey, Luke Flynn, Eric Pilger, Scott Ginoza, Mark Wood, Lance Yoseshige, Gabriel Guererro, Lucas Anderson, Charles Swenson, Sachidananda Babu

Small Satellite Conference

The Hyperspectral Thermal Imager 2.0 (HyTI-2) is a next-generation long-wave infrared (LWIR) hyperspectral imaging payload designed to operate as a continuously sensing, onboard intelligent node on a small satellite platform. Building on the heritage of the original HyTI mission, HyTI-2 delivers advances in spectral and spatial performance, onboard processing capability, and operational duty cycle, enabling sustained operational capability to support low-latency, data-rich Earth observation architectures for future satellite constellations. As the primary payload of the NASA ESTO InVEST-funded Active Cooling for Multispectral Earth Sensors (ACMES) mission, HyTI-2 is scheduled to launch in 2027 to a 550 km sun-synchronous orbit. HyTI-2 …

Optimization Of Orbit-Maintenance Strategies For Small Satellites In Cislunar Space, Timothy Lauinger, Bradley Cotten, Robert E. Zee

Small Satellite Conference

Renewed interest in lunar exploration and the development of a sustained cislunar economy has driven demand for low-cost missions supporting mapping, communications networks, navigation services, and scientific studies. Recent growth in rideshare opportunities to the Moon has made small-satellite architectures a viable and cost-effective approach for these missions. Successful execution of these missions, however, depends critically on fuel-efficient and reliable orbital insertion and maintenance strategies, as cislunar missions impose substantially higher delta V requirements than low-Earth orbit missions due to the inherent instability of low lunar orbits. Perturbations arising primarily from lunar mass concentrations drive secular growth in orbital eccentricity …

A Feasibility-Aware Attitude Trajectory Planner For Small Satellites, Patrick Mckeen, Niclas Scheuer, Kerri Cahoy

Small Satellite Conference

Spacecraft attitude control traditionally requires extensive per-mission engineering—hand-tuned gains, mission-specific mode logic, and conservative operating envelopes—that breaks down when on-orbit conditions deviate from ground assumptions. This is especially costly for small satellites, where limited ground support makes autonomous adaptability essential. We present a feasibility-aware attitude trajectory planner that replaces this hand-engineered stack with continuous planning from a digital twin: less a new feedback law than a different division of labor, in which the mode logic, gain tuning, and desaturation a conventional ADCS builds as separate pieces are instead absorbed into a single optimization.

Built on the ALTRO trajectory optimization algorithm, …

Nasa Stari Mission: A Formation-Flying Pathfinder For Space Interferometry, Akshat Dubey, Caden Burkhardt, Raven St. Clair, Austin Thomas, Tobey Chang, Shivani Sunil, Jacob Klingler, Bradley Bialke, Hannah Cherry, Adrien Boissy, Yethinder Ragav Lakshmi Kumar, Daniil Voloshin, Michael Meyer, John D. Monnier, James W. Cutler, Ethan Foss, Samuel Y. W. Low, Antonio Rizza, Simone D'Amico, Althea Noonan, Mark Gorrow, E. Glenn Lightsey, Melissa Flores, Alexa Lapinta, Albert Ostoja-Starzewski, Leonid Pogorelyuk, Gautam Vasisht, Kerri Cahoy

Small Satellite Conference

The STarlight Acquisition and Reflection toward Interferometry (STARI) mission is a NASA-funded two spacecraft 8U CubeSat technology demonstrator currently in Phase B designed to advance key capabilities required for future space-based optical interferometers. STARI will demonstrate end-to-end beam transfer by reflecting starlight from one spacecraft to another and injecting the received beam into a single-mode optical fiber when it launches in 2029. Formation flying and transferring starlight at very close proximities (25-200 m) presents GNC challenges such as collision safety, precision position control, and fast, precise beam control. The mission ConOps along with a sophisticated GNC system enables passively safe …

Model To Predict Solar Eclipse Impacts On Cygnss Mission Operations, Zach Wiens, Jillian Redfern, Amanda Alexander, Brian Magee, Sam Jones, William Wells, Caden Gobat

Small Satellite Conference

Launched into low-Earth orbit in 2016, the Cyclone Global Navigation Satellite System (CYGNSS) mission is a constellation of eight small satellites that studies hurricanes and soil moisture. The spacecraft orbit in a fixed orientation with the instrument pointed nadir and the main solar array pointed zenith. During high beta angle seasons – periods during which the magnitude of angle between the Sun vector and the orbit plane is large – the solar arrays generate less power, so mission operators roll the spacecraft 10-16° towards the Sun. This maintains the battery state of charge above the safe-mode threshold. After nine years …

Software Defined Swarms, Nathan Benz, Scott Miller, Jeff Huang, Sonny Hwang, Todd Sarshad, Edmund De La Cruz, Thomas Magesarcher

Small Satellite Conference

The Starling Extended Mission has demonstrated the transformative potential of software-defined architectures in multi-spacecraft swarms. Building on the original Starling mission, which validated autonomous coordination and networking among small satellites, the extended phase focused on adaptability—updating onboard payload software and software-defined radios (SDRs) to enable entirely new experiments without hardware modifications. This capability signals a new approach: spacecraft swarms can evolve post-launch to meet emerging scientific and operational objectives. 

Central to this extension was the deployment of new software enabling two-way ranging and “reverse GPS” source identification using raw radio frequency (RF) signals. Traditionally, ranging and navigation rely on pre-integrated …

The Space Cognitive Network: From Fractionated Spacecraft To Collaborative Ai-Enabled Space Infrastructure, Owen Brown, Dennis Gatens, Fred Kennedy, John Moberly, Rusty Thomas, Derek Tournear

Small Satellite Conference

Over the past two decades, small satellite architectures have undergone a fundamental transformation — from platform-centric spacecraft, to globally distributed data-centric constellations. This paper traces that evolution and argues that a third shift is now underway: cognition-centric space architectures enabled by artificial intelligence (AI) as infrastructure. 

We begin by revisiting one of the earliest disruptive space architecture concepts: the fractionated satellite. Developed at the Defense Advanced Research Projects Agency (DARPA) in the mid-2000s, the fractionation concept decomposes a monolithic spacecraft into distributed elements. While the original vision emphasized physical subsystem decomposition, the System F6 program ultimately revealed that the greatest …

Sar Disksat Demonstration Mission For Constellation In Vleo, Hirobumi Saito, Mitsuteru Kaneoka

Small Satellite Conference

We proposed a novel concept of quasi-two-dimensional SAR (synthetic aperture radar) satellites, SAR DiskSats, in 2023 at this conference. This year, in 2026, the demonstration missions of SAR DiskSats are authorized by the Japanese government as a Space Strategy Fund’s Mission. This paper describes the concept and the mission scenario of the demonstration mission in 2028 and 2030. The SAR DiskSat features a deployable passive slot array antenna that can be compactly folded within the quasi-two-dimensional satellite body. This configuration allows for flexible solar cell sheets to be installed on the backside of the antenna, as the antennas do not …

Design Mechanism Framework For Autonomous Small Satellite Constellations – A Newspace Outlook, Mohammed Irfan Rashed

Small Satellite Conference

The increasing deployment of small satellite constellations is driving a transition from isolated spacecraft missions toward distributed and coordinated space operations. However, as constellation size and mission complexity grow, traditional ground-centric operational approaches become difficult to scale due to communication limitations, delayed decision-making, and increased operational workload. While autonomy has been widely explored through onboard algorithms and artificial intelligence techniques, there remains limited focus on how autonomy should be integrated into the systems engineering architecture of constellation missions. This paper presents a Design Mechanism Framework (DMF) for autonomous small satellite constellations that embeds autonomy directly into mission architecture, operational logic, …

Satellite Constellations 2026 - Survey, Trends And Economic Viability, Erik Kulu

Small Satellite Conference

This paper presents the commercial satellite constellation landscape as of Jan 1, 2026. It is based on data from the public NewSpace Index (www.newspace.im), which has tracked commercial constellations since 2016 and contained 456 entries by the end of 2025. 

Many constellation operators have launched initial satellites or small batches, but only a few have reached regular launch rates. Deployment has generally been slower than announced, with many projects scaling back plans or delaying timelines. SpaceX has a significant lead, having launched more than 11,000 Starlink satellites. The next largest commercial operators, Planet and OneWeb, remain well below 1000 satellites. …

Small Satellite Launches From Japan: Zero Launch Vehicle And Hokkaido Spaceport, Atsuta Keiji, Masaki Fujii

Small Satellite Conference

INTEGRATED LAUNCH SYSTEM

• Easy access to factory in case of last minute iterations
• Simplified logistics
• Launch site is tailored made for ZERO

High-Torque Reaction Wheels For Agile Small Satellites, Thomas Brunsgaard, Matt Carton, Kearney Lackas

Small Satellite Conference

Blue Canyon Technologies has developed a high-torque reaction wheel (RW) product line to meet the growing attitude control demands of next-generation small spacecraft. As small satellites expand into missions requiring rapid retargeting and precise pointing, spacecraft agility is foundational to mission performance. More targets equal more data collection, translating to greater mission insight and revenue generation. 

This paper describes Blue Canyon’s approach to product line architecture that enabled rapid development and deployment of high-torque reaction wheels across multiple size classes. The high-torque variants deliver 0.5 Nm of torque, representing a 2X increase over standard configurations with 60% of the baseline …

Shining A Spotlight On Maritime Dark Traffic, Alex Da Silva Curiel, Darren Jones, Rob Knight, Rupert Taylor, Leo Jofeh, Sir Martin Sweeting, Per Atle Våland, Simon Flack, Patrik Mandelin, Håkon Heier

Small Satellite Conference

The ability to support Maritime Domain Awareness from space using Synthetic Aperture Radar (SAR) has been successfully demonstrated in the past, however practical challenges in achieving the necessary area coverage, temporal coverage and spatial resolution for a practical system has eluded wider adoption. Yet demand for Maritime Surveillance has increased in recent years, to protect important maritime energy and communications infrastructure, fisheries, and maritime reserves, and especially for maintaining national security and territorial integrity. A novel approach to the SAR payload design solves these challenges, and smallsat technologies have also matured to the point where a High-Resolution Wide-Swath (HRWS) system …

Development Of Piezo Fast Steering Mirrors For Fso Inter-Satellite Communication, Frank Claeyssen, Arnaud Gilson, Thomas Maillard, David Ferris, Xavier De Lepine, Oliver Sosnicki, Jocelyn Rebufa, Clément Cote, Francis Bortolaso, Pascal Mexe

Small Satellite Conference

To allow faster communication between satellites, Radio Frequency (RF) links are being replaced by laser optical links, often called Free-Space Optical Communication (FSO). Each satellite embeds several optical communication terminals (OCT), each one needing two Fast Steering Mirrors (FSM) for laser beam fine and fast steering. Thus, for some giant constellations, the total number of FSM can reach up to 100 000 FSM. This New Space market induces not only technical challenges, such as good SWaP, but also industrial challenges, in particular reproducibility, cost-effectiveness and low cost of ownership vs Orbit segment. To address these various FSM needs, CEDRAT TECHNOLOGIES …

Cubesat Led Transmitter For Optical Communication Downlink, David Hinkley, Sam Pedrotty

Small Satellite Conference

The CubeSat radio frequency (RF) spectrum licensing step has always been long and therefore stressful to developers. With more satellites entering orbit, spectral congestion in the available RF frequency bands has become a problem. An optical-only solution eliminates this problem and provides a path for a lower power and higher throughput data link. The risk of a weather outage drives a solution that requires enough geographically diverse optical ground locations that a clear line-of-sight is always available. The Aerospace Corporation, with funding from NASA, has developed a CubeSat light emitting diode (LED) transmitter and an inexpensive commercial portable optical telescope …

Asynchronous One-Way Range (Aowr) – Alone Positioning And The Applications, Junichiro Kawagichi, Shingo Nishimoto

Small Satellite Conference

The paper first reports the recent operational results of the HOKUSHIN satellite. It explains how our extended code correlation method has performed and provides link threshold information, specifically the demonstrated C/N0 figures. The paper next focuses on cis-lunar space applications, beginning with direct AOWR-alone positioning directly from Earth using three or more small-aperture ground stations. The application employs a ‘Self-Positioning’ strategy. This system operates in cis-lunar space with 3-meter-class ground stations and CubeSats larger than 6U in size equipped with 200x300 mm patch-array antennas on. It enables universities and startups to conduct genuine lunar exploration. The team won the Strategic …

Flight Test Of The Autonomous Navigation, Guidance, And Control (Autongc) Software On The Starling Swarm, Robert Pritchett, Nathan Stacey, Sun Hur-Diaz, Michael Romeo, Nickalas Cason, Katherine Fowee Gasaway, Nathan Esantsi, Behnam Azimi, Sean Semper, Hossein Mohammadkhan, Grant Hecht, Joseph Patton, Liam Greenlee, Justin Clavette, Alan Cudmore, Ian Hammer, Ted Hendriks, Terry Stevenson, Nahum Alem

Small Satellite Conference

Performing real-time autonomous guidance, navigation, and control (GN&C) functions onboard spacecraft is critical for enabling greater spacecraft autonomy. The autoNGC (autonomous Navigation, Guidance, and Control) software suite is a collection of applications, built on the NASA core Flight System (cFS), that provides these capabilities. This paper presents results from the first flight demonstration of autoNGC, conducted on the NASA Starling mission in 2025. The Starling spacecraft's use of cFS enabled autoNGC to be uplinked and run onboard despite the spacecraft already being in orbit. The flight test had three goals: to demonstrate onboard GPS navigation, onboard state and uncertainty prediction …

Ai For Autonomous Operation Of Small Satellite Missions, Lucy Donnell, Reuben Lynch, Charlotte Crawshaw, Karl Buckley, Robert Field, Steven Kay

Small Satellite Conference

UK space industry partners Craft Prospect Ltd (CPL) and GMV deliver an advanced avionics demonstrator which incorporates cutting-edge machine learning (ML) techniques to enhance on-board autonomy for small satellite space missions. The work is funded by the European Space Agency (ESA), and the delivery partners combine expertise in embedded Artificial Intelligence (AI) and space systems engineering to target use cases for on-board autonomy which offer the best gains for a diverse range of mission types including institutional and commercial Earth observation (EO), navigation, scientific, and lunar exploration missions.

Common technical target applications have emerged as underpinning technologies which enable the …

Multiclass Satellite Payload For Sar, Leonardo Carrer, Davide Giudici, Fabio Gerace, Paolo Falcone, Davide D'Aria, Giuseppe Leccese, Vincenzo Pulcino

Small Satellite Conference

SAR enables reliable all-weather, day-and-night Earth observation. Conventional SAR missions rely on large satellites, high power and costly development cycles.

NanoSat and SmallSat platforms offer faster deployment and lower mission costs, but face strict mass, volume, power and antenna constraints.

A modular multiclass payload allows the same SAR electronic core to be adapted to different satellite platforms.

Distributed SIMO/MIMO operation shares Radar resources across multiple spacecraft, improving scalability, resilience and revisit time. The proposed architecture enables high-performance X-band SAR missions using compact and cost-effective satellite systems.

Vpx/Sosa Systems: Enabling Multi-Vendor Interoperability, Novo Space

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Probe Cytotoxic And Oxidative Stress Effects Of Nanoplastics On Caco-2 Cells: Insights From Raman Spectroscopy And Machine Learning, Bryan Gustafson, Negar Kosari, Emily Brothersen, Morgan Mosher, Anhong Zhou

Biological Engineering Student Research

Nanoplastics and microplastics have become an increasing ecological and health concern due to their widespread presence in the environment and food chain. In this study, Caco-2 cells were used as an in vitro model of the human intestinal epithelium to investigate the cytotoxic effects of polystyrene nanoparticles and microparticles of varying sizes, concentrations, and surface modification. Oxidative stress and apoptosis were evaluated following particle exposure. Raman spectroscopy, combined with machine learning analysis, was employed to detect and characterize biochemical alterations in the cells. Several peak ratios were selected to cluster data depending on size. A correlation between apoptosis and both …

831sat: A Cubesat Subsystem Platform For Space Systems Development Education, Dominic S. Fucile, George Lordos, James Dingley, Kerri Cahoy, Paul Fucile

Small Satellite Conference

The CubeSat standard has become one of the most popular frameworks for co-curricular and extracurricular student satellite projects, yet its integration into formal curricula for space systems engineering remains limited.

Accessibility concerns:

• Students encountering satellite design for the first time face a learning curve when working with flight-representative hardware.
• Time constraints of undergraduate semesters limit the technical depth covered in a single course.
• Existing educational platforms often lack subsystem flexibility and fidelity needed to deliver an authentic systems engineering experience.

Presented is the 831Sat, a custom single board platform that provides core satellite subsystems:

• Central Processing Unit
• Electrical Power System …

Design And Implementation Of A Semi Automated Uhf Ground Station For Small Satellite Missions: A Case Study From India, Binoop Joseph, Vinayak Manoj, Thomas Francis, Madhav Vinod, Nikhil Jacob, Salih Majeed, Prajin I. R., Meghana Suresh, Salman Al Fariz K., Sijo George, Anish Chandra B. S., Anamika Kamath, Anjay Sudesh, Anurag Reghu, Aravind M. B., Manu Mohan, Ashfaque K. P., Amal Chandran

Small Satellite Conference

Mission success ultimately depends on reliable telecommand and telemetry links between spacecraft and Earth. For small satellites operating under tight power, size and link margin constraints, a technically robust and regulation compliant ground station is a mission critical enabler rather than an afterthought.

This poster presents a case study of a semi automated UHF ground station designed, built and commissioned by HEX20 in Thiruvananthapuram — one of the earliest privately owned and operated satellite ground stations in India — covering the hardware signal chain, the tracking and decoding software stack, integration and calibration, and the regulatory path to operation.

Modeling Liquid Propellant Slosh Disturbances For Small Satellite Attitude Control, Phillip Miret, Nathan Cole, Robert E. Zee

Small Satellite Conference

Objective:

Develop and optimize a reduced order spring-mass-damper (SMD) analogue of propellant slosh using computational fluid dynamic (CFD) analysis. Evaluate the efficacy of generating feedforward compensation terms using the SMD model to improve attitude control performance during rapid spacecraft slews.

Multipoint Sensor Constellations Demonstrated On Spear-1 Using Radstar, Black Box, And Fastbus+, Jeff Dailey, Matt Orvis, John Pugsley, Matt Voss, Hank Voss, Nathan Turner, Dillon Embry, Gretchen Barnes, Mike Schuckel, Nathan Daniels

Small Satellite Conference

NearSpace Launch (NSL) has developed and flown both multipoint sensor constellations and hosted-payload smallsat constellations since 2014, supporting missions for educational, commercial, and government partners. These missions enable distributed, multipoint sensing by combining compact sensor suites with persistent, low-latency satellite links and a common, time-ordered data architecture suitable for constellation operations. Recent flight heritage includes 24/7 space-to-Internet communications and rapid Launch and Early Operations Phase (LEOP) telemetry acquisition to support early identification, commissioning, and anomaly response. Most recently, the Space Power and Energy Advanced Reconnaissance (SPEAR-1) constellation demonstrated this multipoint architecture while maturing advanced power-generation and energy-storage technologies relevant to …