Digital Commons Network^™

Energy-Aware Dynamic Tasking For Earth Observing Satellites With Deep Reinforcement Learning, Nicholas Nordlund, Tim Upthegrove, Leandros Tassiulas

Small Satellite Conference

Dynamic tasking for agile Earth-observing satellites (AEOS) adapts preplanned schedules using onboard lookahead sensors to detect cloud cover that obscures targets. Existing approaches decompose tasking into sequential lookahead, maneuver, and capture stages, limiting their ability to manage tradeoffs over long time horizons. Instead, we formulate dynamic tasking as a constrained partially observable Markov decision process (CPOMDP) and introduce Cloud-Aware Dynamic Earth-observation Tasking (CADET), a deep reinforcement learning (DRL) framework that jointly selects maneuvering and sensing actions under resource constraints. We derive a closed-form model for the probability that a target is visible given a spatially aggregated lookahead observation, …

From Estimation To Certainty: Enhancing Smallsat Constellation Replenishment Planning With Physics-Based Solar Forecasting, Scott W. Mcintosh, Katherine Monson, Carolyn Belle, Chris Habib, Brianna Aubin

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

First Generation Of Project A.S.P.I.R.E. – A 1u Cubesat Mission For Technology Demonstration And Student Involvement In New Zealand, Shuanghui Zhao, Shunxing Shi, Kristen Lian, Rose Peens-Hough, Arami Peens-Hough, Changrui Wang, Joowon Hwang, Jerry Sun, Edward Sun

Small Satellite Conference

MOTIVATION

A feasibility study conducted at an Auckland secondary school in December 2024 found strong interest in satellite-related learning. Following an outreach presentation, 63 students (Majority aged 15 - 18) completed a questionnaire, with an average interest rating of 4.86/5. The most popular subjects were Orbital Physics, Mathematics, Mechanical Engineering, and Electrical Engineering (fig. 1).

Mission Orientated Flight Software Development: Cubestep, Tirth Thakkar, Howard Lee, Viren Kumar, Maranda Laws, Shridhi Seth, Marco Maggia, Navid Nakhjiri

Small Satellite Conference

Small satellite teams often develop flight software and mission operations separately, leading to software behaviors that drift out of sync with ground procedures. To fix this, we present a co-design approach that directly links mission goals and operational procedures to the onboard flight software architecture. Demonstrated on the CubeSTEP-Cerberus mission using NASA’s F′ framework and FreeRTOS, our system maps mission intent into five constrained software states (Initialization, Safe, Idle, Experiment, and Transmit) guarded by automated health checks. This co-design strategy ensures the spacecraft acts autonomously to preserve its goals while strictly maintaining operator control over critical decisions.

Planet's Next Generation Evolution Of The High Speed Radio: 10 Gbps Smallsat Radio, David Nemeth, Kiruthika Devaraj, Varun Sharma, Timothy Kordas, Gil Michael, Stefan Turkowski, Abhra Dasgupta

Small Satellite Conference

Planet is a vertically integrated aerospace and data analytics company that operates the world’s largest commercial fleet of remote sensing satellites. Our mission is to image the whole world every day, and make change visible, accessible, and actionable. We have launched over 600 satellites and built up an automated mission control and ground station infrastructure to monitor and control the satellites, and download the imagery data. Planet’s agile aerospace philosophy of rapid prototyping, iteration, and adaptation of the latest commercial-off-the-shelf (COTS) technology has allowed for continuous improvements in data throughputs on our High Speed Downlink radio. Planet’s HSD2 achieves greater …

Modular, Scalable Electroadhesive Technology For Rapid Response Satellite Servicing And De-Orbit, Kalia Crowder, Victor Agüero

Small Satellite Conference

Building on previous surface attachment testing and a study of the Cambrian Works Space Payload for Inertial Despin Efficient Effects (SPIDEE) architecture carried out under AFRL support, this work presents a modular, scalable electroadhesive attachment architecture enabling rapid-response satellite servicing and de-orbit missions. Prior test and analysis campaigns provided quantified performance validation across the small satellite size range, from 3U CubeSats to ESPA-class platforms, demonstrating the scalability required for diverse time-critical servicing scenarios.

Testing validated performance under representative on-orbit conditions and dynamic scenarios. Attachment force measurements across spacecraft materials representing aluminum bus structures, composite panels, multi-layer insulation, and solar cells …

Design, Qualification, And Implementation Of Modular Spacecraft Radio Testing Enclosures For Small Satellite Missions, Dexter Stewart

Small Satellite Conference

As small satellite missions evolve, spacecraft platforms increasingly integrate radio-frequency (RF) antennas to support telemetry, command, and inter-satellite communication links that must be verified following full system integration. Recent changes in launch site safety policy, most notably SpaceX’s ban on over-the-air (OTA) testing, have created a critical gap in the ability to qualify spacecraft communication systems during testing at the launch site. This paper presents the design, qualification, and implementation of modular RF containment enclosures, known as ’antenna hats’, developed to enable safe, non-OTA testing of fully integrated small satellites. The antenna hats are self-contained enclosures that interface directly with …

Beyond Parametric Adaptation: Periodic Redesign For Reaction Wheel Degradation In Precision Pointing Cubesats, Bruno Ingrao

Small Satellite Conference

CubeSat missions increasingly require sustained science-grade precision pointing over long durations. Although sub-arcsecond line-of-sight (LoS) stability is achievable, maintaining this performance is challenged by nonlinear, speed-dependent, and time-varying reaction wheel behavior. As actuator degradation progresses from beginning-of-life (BOL) to end-of-life (EOL), model-plant mismatch can lead to significant pointing degradation and potential loss of mission capability. This work investigates the limitations of fixed-gain and parametric adaptive control under degraded actuator conditions and proposes a periodic identification and controller redesign framework. The approach detects persistent model mismatch using innovation-based consistency and performance metrics, triggers on-orbit identification, and updates the actuator model using …

Citizen Science As A Long-Term Environmental Baseline: Assessing Impacts Of A Small Dam Removal In Montana, Usa, Bethany Blakey, Natalie Bursztyn

Watershed Sciences Student Research

As dam removals increase in frequency across Europe and North America, most research has focused on the impact of larger dam removals, despite the removal of small dams being much more common. There are hundreds of small dams in Montana, USA, and this research investigates impacts on stream ecology and morphology using citizen science data collected over eight years spanning before and after a 2020 small dam removal in Rattlesnake Creek. We analyzed pebble count grain size distributions and aquatic macroinvertebrate biotic indices from 2017 to 2024 to assess changes in sediment transport and macroinvertebrate population as well as evaluate …

Comparative Analysis Of Reaction Wheels And Control Moment Gyroscopes For High-Capacity Orbital Data Centers In Sun-Pointing Mission Profiles, Chih Ta Wu, Po Hsun Yen, Jen Hao Cheng, Kai Kuo Liao, Shang Jung Lee

Small Satellite Conference

• Orbital data centers (ODCs) are moving from concept to near-term engineering: Starcloud (5 GW), Meta / Overview Energy (1 GW SSP), SpaceX (up to 1M-satellite FCC filing).
• Multi-kW to GW-class compute demands solar arrays of unprecedented scale → extreme inertia and disturbance torques.
• Can Reaction Wheels (RWs) vs Control Moment Gyroscopes (CMGs) hold an ODC in a sun-nadir pointing profile?

Optical Advantages In Using Extremely Stable Materials In Small Satellite Telescopes, Tony Hull, Jesse Bonfeld, Dustin Ruth, Florian Gollier, Janina Krieg, Thomas Westerhoff, Jacqueline Caraballo

Small Satellite Conference

Small-satellite telescopes experience continuous thermal transients from changing Sun and Earth view factors plus CONOPS → temperature gradients T(xi) → distort mirrors/metering if the material is sensitive to temperature.

Transients are partially mitigated by diffusivity, but only with uniform temperature changes. Orbital and CONOPS transients are not uniform → The architect must examine the material response to realistic transients and gradients.

Optimal optical performance is supported by appropriate passive material attributes!

Swap: An Ai-Enabled Cubesat For Low-Latency Space Weather Alerting, Miles H. Currie, Douglas Franz, Paul Kocyla, Omar Sharaf, Sarvesh Garimella

Small Satellite Conference

1 — Background

• Growing dependence on space-based assets (telecom, transport, grid, GPS) = growing space-weather exposure
• A Carrington-class storm today would mean cascading failures and losses in the trillions
• Current assets (e.g. GOES, ACE, DSCOVR) are excellent but large, costly, and with minutes to hours of alert latency from ground processing; weak coverage off the Earth–Sun line, where multi-point views could untangle the solar flare/SEP/ CME chain
• The Space Weather Alerting Platform (SWAP) concept mission (right) is a low-cost, 3U cubesat solution for proliferated solar monitoring with low-latency onboard AI alerting

Toward Public Access To On-Orbit Propulsion Data From Equuleus: Preparing Real Flight Data For Community Use, Hiroyuki Koizumi, Isamu Moriai, Hokuto Sekine, Keita Nishii, Mariko Akiyama, Shintaro Nakajima, Yosuke Kawabata, Yasuho Ataka, Shunichiro Nomura, Ryota Fuse, Ryu Funase

Small Satellite Conference

EQUULEUS is a 6U lunar exploration CubeSat, jointly developed and operated by the University of Tokyo and the Japan Aerospace Exploration Agency (JAXA). It was launched in November 2022 by the Space Launch System (SLS) into a lunar transfer orbit and achieved insertion into a trajectory toward the Earth–Moon Lagrange region through multiple lunar flybys using its onboard water resistojet propulsion system AQUARIUS. The EQUULEUS primary mission is the demonstration of trajectory control technology in the Sun-Earth-Moon region for the first time by a nano-spacecraft.

Zerodur®: Comprehensive Data Enables The Reliability Of Evidence-Based Design, Dustin Ruth, Florian Gollier, Jesse Bonfeld, Dustin Ruth, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

ZERODUR® is a glass-ceramic formulated for high-performance optics under imperfect temperature control. Crystallites in a glass matrix balance expansion: crystals shrink while residual glass expands, preserving geometry at fine scale.

This yields the lowest passive thermal response of any optical material-enabling high-contrast, high-resolution, low-scatter imaging and minimal transmission leakage for SmallSat telescopes.

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 …

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 …

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 …

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 …

Dante: A Spaceborne Radar Constellation For Debris Detection And Tracking, Leonardo Carrer, Davide Giudici, Bernhard Niedermayer, Christian Federspiel, Wolfgang Ebner, Robert Greinecker

Small Satellite Conference

The growth of space debris in Low Earth Orbit (LEO) is increasing collision risk and challenging the sustainability of space operations, while current ground‑based radars remain limited in sensitivity, coverage and update rates especially for small objects. This paper presents DANTE (Detection ANd Tracking of space dEbris), a spaceborne radar constellation concept designed to enhance debris detection, tracking and orbit refinement directly from LEO. DANTE employs multiple low‑cost satellites equipped with X‑band phased‑array radars operating in two modes: a Tracking Mode for trajectory refinement of known objects and a Beam‑Park/Electronic Fence Mode for debris discovery. Performance analyses indicate sub‑meter resolution …

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 …

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. …

Development And Pre-Flight Verification Of The 6u Cubesat Vertecs For Extragalactic Background Light Observation, Ryo Hashimoto, Kei Sano, Takao Nakagawa, S. Matsuura, A. Takahashi, K. Takimoto, K. Tsumura, J. R. Cordova-Alarcon, V. H. Schulz, N. C. Örger, D. Nakayama, E. E. Areda, R. J. G. Rosales, T. Fuse, K. Hamada, Y. Otani, B. V. H. Kumar, K. A. Hil, A. R. S. Islam, T. Tome, Y. Yasudao, C. Narongphun, S. Nakagawa, H. Tanaka, Y. Hirose, Y. Iwaki, A. Ikeda, A. Ojika, Y. Oohara, A. Tsumoto, K. Kurosaki, E. Fukumoto, C. Arakawa, H. Masuno, A. Oho, M. Ebisu, I. Jikuya, M. Cho, H. Masui, H. Matsuhara, N. Isobe, Y. Miyazaki, S. Ikari, Y. Yatsu, T. Wada, R. Funase, K. Hirako, R. Hirose, Y. Ofuji Aoyanagi, T. Goto, T. Hashimoto, V. V. V. Rao, C. Wu

Small Satellite Conference

The extragalactic background light (EBL) (Fig. 1) is the diffuse light arriving from outside our Galaxy. Previous studies revealed that the near-infrared EBL is several times brighter than the integrated galaxy light (IGL).

This excess may originate from the first stellar objects in the early universe or from intrahalo light. Their spectra differ in the visible range (Fig. 2), so the visible EBL is the key to identifying the origin.

Ground-based observations are contaminated by foregrounds such as airglow. We therefore developed VERTECS (Visible Extragalactic background RadiaTion Exploration by CubeSat) to observe the EBL from space.

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 …

Nasa's Small Spacecraft & Distributed Systems: Development And Demonstration Of Technologies Enabling Swarms And New Spacecraft Platforms With Ai And Edge Computing, Jan Stupl, Rodolphe De Rosee, Samson Phan, Michael Gaunce, Bruce Yost, Craig Burkhard, Edward Tagalicud, Roger Hunter, Christopher Baker, Justin Treptow-Miller, Sasha Weston, Luke Idziak, Julianna Fishman, Dorothy Santos

Small Satellite Conference

NASA’s Small Spacecraft & Distributed Systems (SSDS) within the Research and Technology Mission Directorate (RTMD) expands U.S. capability to execute unique missions through targeted investment, rapid development, and flight demonstration of small spacecraft technologies applicable to exploration, science and the commercial space sector. SSDS strategically invests in technology development and on-orbit demonstrations executed across NASA, other government agencies, industry, and academia. The program’s University SmallSat Technology Partnerships initiative awards academic researchers with the opportunity to collaborate with NASA to mature innovative technology. Capabilities aligned with RTMD’s technology shortfalls and interests - power, processing, propulsion, sensors, communications, autonomous navigation, architectures, and …

Intelligence Where Data Is Born: Vision Transformer-Based On-Orbit Change Detection For Earth Sensing, Matthew Morabito, Faries Tadros, Catherine Ordun, Michael S. Sellers, Daniel Wald

Small Satellite Conference

This paper introduces a model framework for autonomous hyperspectral segmentation that couples a foundation model with a supervised segmentation head to enable compact, high performance on-orbit scene understanding. This approach is designed to deliver end-to-end onboard processing, inference, confidence scoring, and prioritization so the spacecraft performs interpretation at or near image collection time and minimizes downlink usage by transmitting only high-value or high-interest outputs rather than full image streams. A key design element is adaptive intelligence over mission lifetime: low-size, over-the-air partial models updates as small as kb-scale enable post-launch retuning and mission-specific refinement without GB-scale data transfer. By reusing …

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 …

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 …

Schott Options For Efficient Design-To-Cost Zerodur® Optical Assemblies With Established Supply Chain Reliability, Florian Gollier, Jesse Bonfeld, Dustin Ruth, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

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.

Lego®-Based Cubesats For Space Outreach, Stefan Brandle, Joshua Brown, Evan Smith, Drew Nye, Sydney Reddy, Twidy Kwae, Kaiya Grzesiak, Matthew Roderer, John Hetz

Small Satellite Conference

Taylor University Computer Science and Engineering is building a satellite having a LEGO®-robotics-based payload.

Mission Goals

• Have university students build a novel ELEO satellite
• Demonstrate viability of LEGO robotics electronics in space for short-term low-altitude missions
• Enhance space awareness by capturing the public's imagination through integral use of LEGO in an actual satellite
• Identify partners willing to provide advice and promote this project
• Create additional pathways for K-12 and university student participation in building satellites and satellite-related projects
• Support other space-education organizations through a high-visibility satellite project
• Continue space outreach efforts in the spirit of the ThinSat project
• ThinSat was …