Digital Commons Network^™

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.

An Operator-In-The-Loop Smallsat Operations Simulation For Classroom Training, Samuil Nikolov, Kaelyn Tindall, Lana Laskey

Small Satellite Conference

Training spacecraft operators through a hybrid environment combining live telemetry, game-engine visualization, subsystem consoles, and real-time anomaly response.

An End-To-End Optical And Ethernet Networking Architecture For Next-Generation Satellite Constellations, Gianluca Giuffrida, Francesco Falaschi

Small Satellite Conference

• Modern satellites generate ever-increasing data volumes, increasingly challenging traditional RF links. IngeniArs combines very high speed optical links, up to 10 Gbps, with an onboard Ethernet routing fabric
• Optical data is packetized and dynamically routed for onboard storage or processing, or relayed across the constellation from satellite to satellite until it reaches an available ground station
• The result is reduced time-to-ground, increased contact opportunities, and more resilient end-to-end data delivery across the space and ground segments, despite intermittent link availability

Feasibility Of Failure-Resilient Swarm Formation Flying And Multi-Beam Coherent Apertures In 10000+ High-Density Satellite Swarms, Sumio Morioka

Small Satellite Conference

Direct-to-Device (D2D) communication links satellites directly to ground terminals without large antennas, supporting future Cyber-Physical Systems (CPS) and IoT. Our earlier work [1] showed that a formation of 10,000+ ultra-small satellites, as a coherent phased-array aperture, closes the D2D link budget. This study asks whether the formation can be operated within each satellite’s available power.

Validation Of A Modular Adcs Architecture For Small Satellites, Saish Sridharan

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

Magnetic Balancing For Microvibration Reduction In Passive Magnetic Bearings For Smallsat Reaction Wheels, Deckers Niel, Baekeland Mante, Cuypers Cedric, Seiler Rene, Vandepitte Dirk, Delabie Tjorven

Small Satellite Conference

Reduction and mitigation of microvibrations constitutes a crucial field of interest in the research of spacecraft reaction wheels. This applies all the more so in small satellites, where even minimal sources of vibrations lead to imprecision of onboard instruments. To address this, magnetic bearings offer contactless support, and thus prevent several sources of microvibrations that exist in classical ball bearings, for instance the mechanical imperfections in rolling elements. The inherently low stiffness of magnetic bearings also significantly reduces the transmitted forces in reaction wheels. Another advantage of contactless support is its potential longer lifetime because of the absence …

Manufacturing Advances For Cost Effective, Large Aperture Monolithic Telescopes, T. Suratwala, R. Steele, G. Tham, J. Ross, J. Johnson, O. Herrera, M. Cahill, D. Bechtold, R. Bechtold, F. Ravizza, J. Cortes

Small Satellite Conference

Space has become increasingly more contested over the last decade, with the proliferation of satellites and space assets that require new levels of Space Domain Awareness (SDA). Space is often described by the US Government as the next warfighting domain. Control, understanding and dominance over this vast domain requires exquisite and complex optomechanical systems.

Lawrence Livermore National Lab’s Space Science and Security Program (SSSP) has developed unique monolithic optics, which are ground-aligned during manufacturing and are nearly athermal. These qualities greatly reduce the complexity of the optical payload when compared to legacy telescope designs. Monolithic optics deliver excellent imaging capabilities, …

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 …

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.

Rad-Hard Circuits For Complete System-On-Chip Integration Of Smallsat Electronics On Standard Non-Rad-Hard Cmos Including Finfets, Ignatius Bezzam, Dhandeep Challagundla, Riadul Islam

Small Satellite Conference

1. SmallSat Compute Is Thermally Constrained

• SmallSats are packing more autonomy, sensing, and payload processing into tighter volumes.
• Power budget, heat removal, and radiation reliability constrain sustained on-orbit computation.
• Off-chip shielding increases mass and volume
• Redundancy and guard-banding increase switching energy. 
• This work targets lower heat generation and higher reliability inside the silicon.

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 …

Systems Progress Overview Of Rosisat: The Radiation Orbital Shielding Investigation Satellite, Chase Patterson, Jacob Blanton, Jayden Mcdonald, Kylie Nager, Colson Walker, Francisco Crespo Cutillas

Small Satellite Conference

Exposure to space weather in the Low Earth Orbit (LEO) space weather environment poses significant challenges to both the integrity and longevity of orbital hardware, as well as the health of astronauts, driving the necessity for improved means of radiation shielding for future manned and unmanned missions. With a 1U CubeSat formfactor, ROSISat is a planned LEO mission that aims to characterize the radiation shielding capabilities of seven candidate materials. By comparing the shielding performance of each composite and constituent material, ROSISat will place a specific focus on correlating how molecular structure influences radiation shielding. Further, current simulations lack the …

Reacquiring Satellites After Unknown Maneuvers In Sensor Blind Spots: A Physics-Informed Behavioral Framework For Closed-Loop Custody Recovery, Naushad Rahman, Niha Agarwalla, Hardik Patel

Small Satellite Conference

Operational problem

After a maneuver during a sensor blind spot, a pre­-gap catalog state may no longer be operationally sufficient. A null look at GS2 must become evidence for where the object could be­ – and where to task next – before access expires.

Scaling Space Power For Small Satellites: Why Manufacturing Capacity Now Matters As Much As Efficiency, Mpower Technology

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

The Quantum Cubesat: A Perspective For Quantum Technology In Orbit, Natalie Pearson, Andrew Kelly, Curtis Talbot, Colin Aitken, Kevin Quillen, Sandy Provan

Small Satellite Conference

Motivation

The ability to measure, control and exploit quantum effects has shown significant potential to outperform classical devices across a variety of applications in computing, sensing and communication. However, quantum devices today typically depend equipment that is large, heavy, expensive and delicate. Bringing quantum capability to space requires a relentless focus on miniaturisation, ruggedisation and applicability. Focusing engineering efforts on the most promising technologies to realise their benefits in orbit is a crucial step in this process.

Validation Of Steering Law For A 4-Variable-Speed Single-Gimbal Control Moment Gyroscope Pyramid Cluster Via Spherical Air-Bearing Testbed, Kai Kuo Liao, Chih Ta Wu, Jen Hao Cheng, Po Hsun Yen, Shang Jung Lee

Small Satellite Conference

• VSCMG: wheel speed is commanded with gimbal rate — the extra DOF lets the cluster slide past singularities.
• HIL: a Helmholtz cage replays the on-orbit field and a solar simulator sets the Sun line.
• This work: HIL validation of a weighted-pseudoinverse steering law, 4-unit pyramid.

University Ground-Station-As-A-Service: Promoting Space It Education And University Collaboration, Daniel Freburg, Will Lewis, Charles Edamala, Phoenix Alpine

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

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

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Zerodur®: Tailoring Opportunities For Your Thermal Environment And Second-Order Optimum Factors, Jesse Bonfeld, Dustin Ruth, Florian Gollier, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

Reinventing The Reaction Wheel, I. Penchev, N. Andrada

Small Satellite Conference

Rapid growth of microsatellite missions and constellations in the 10–600 kg class is increasing the demand for scalable, high-performance attitude control solutions. Advanced payloads for Earth Observation, Synthetic Aperture Radar, complex science missions, and geolocation systems require:

• Low microvibration performance
• Precise pointing stability
• High angular momentum capacity
• Reliable across mission lifetimes

Space Inventor is qualifying a new generation of 1 Nms-class reaction wheels optimized for microsatellite platforms. The innovative mechanical design, combined with manufacturing-aware system design, unlocks expanded performance and mission opportunities for microsatellites and constellations.

Satellite Autonomous Launch Assembly (Satlass): Cold Gas Propulsion System Testing, Anthony Todisco Jr., Jaden Caradine, Justin Della, Essence Howard, Colin Mccaughey, Andrew Hawks, Alexander Kushto, Javier Narvaez, Gabriella Colon O'Hara, Franyerson Lopez Ochoa, Elizabeth Ptak, Diana Tormo, Francisco Crespo Cutillas, Sean Crouse, Lary Finberg

Small Satellite Conference

Project SATLASS plans to become one of the first cold gas propelled CubeSat Deployers used. Using Nitrogen gas, SATLASS will be able to place multiple CubeSats into customizable orbits autonomously. A modular housing unit will allow for 3-1U CubeSats to 1-3U CubeSat to ride along with SATLASS through Low Earth Orbit.

Leveraging Persistent L-Band Leo-To-Geo Relays For The Orchestration Of High-Bandwidth Optical Inter-Satellite Links, Jonathan Maier, Skylar A. Cox

Small Satellite Conference

As the already tremendous demand for data transfer in Low Earth Orbit (LEO) grows, Free-Space Optical (FSO) communication has emerged as a critical capability due to high data rates and inherent resilience attributes. However, the operational complexity of FSO, specifically the Pointing, Acquisition, and Tracking (PAT) process, requires significant operational planning. The narrow beamwidth of optical terminals requires precise spatial coordination, resulting in latency during link establishment, heavy reliance on scheduled ground-based commanding, and an impediment to agile, responsive, and ad hoc operations.

This paper presents a novel orchestration architecture utilizing Viasat’s L-band space relay network as a persistent, always-on …

Evaluating Performance Of Hardware-Accelerated Vessel Detection Algorithms, Michael Tietz, John Warner, Quinton Davidson, Douglas Carssow

Small Satellite Conference

Earth observing satellites contribute to the monitoring of maritime activity by enabling large-scale coverage of open water. For example, spacecraft data can be used to monitor and combat Illegal, Unreported, and Unregulated (IUU) fishing that occurs in coastal and international waters across the globe. However, information latencies limit the utility of space-based sensors for operational users who need real-time situational awareness. These limitations are especially pronounced for small spacecraft with limited power generation and downlink capabilities. In recent years, the devices and tools that enable edge computing and near real-time downlink from small spacecraft have improved substantially. Equipped with these …

Dynaband: Context-Aware Dynamic Band Selection For Onboard Hyperspectral Processing In Small Satellites, Rishigesh Jayananth, Brasen Sheeh

Small Satellite Conference

Hyperspectral small satellites now collect far more data than they can return to the ground. A single acquisition spans tens to hundreds of spectral bands, yet the downlink window on one pass carries only a fraction of it, so operators are forced to drop scenes, bin bands coarsely, or store data that never reaches the ground. Much of this waste is avoidable. When the task is known before the spacecraft images, whether to map water, monitor vegetation, or pick out a mineral signature, only a handful of bands actually carry the answer; the rest is paid for in downlink and …

Metadata-Conditioned Dark-Frame Modelling And Hsdr-Scanfusion Denoising: A Physics-Informed Independent Tool For Low-Cost Hyperspectral Small-Satellite Calibration, Nooh Adnan, Kyaw Thiha, Raffael Gil Dela Cruz, Li Cheng Zheng, Faijul Amin, Areeba Khan, Sameha Tasnim, Sung Jegal, Yunhan Bao, Iliya Shofman

Small Satellite Conference

Hyperspectral imaging in the shortwave-infrared spectrum is valuable for orbital Earth observation, but its use on low-cost, resource-constrained small satellites is limited by thermally dependent dark current, fixed-pattern noise, and intermittent access to matched calibration frames. Traditional mitigation through active cooling, shutters, or frequent dark-frame acquisition can be difficult to accommodate within small-satellite mass, power, volume, and operations budgets. This paper presents a physics-informed independent calibration tool that reconstructs condition-matched dark response from acquisition metadata rather than relying on hardware-heavy calibration at every operating point. The framework combines a stochastic dark-noise simulator, a metadata-conditioned neural dark operator that predicts spectral-spatial …

Design And Performance Of The Active Thermal Architecture Technology For The Upcoming Acmes Mission, Lucas Anderson, Charles Swenson, Miguel Nunes, Robert Wright

Small Satellite Conference

This paper will discuss the basic design, fabrication, and experimental validation plan of the Active Thermal Architecture (ATA), a novel Active Thermal Control (ATC) technology that will be demonstrated on the upcoming Active Cooling for Multispectral Earth Sensors (ACMES) mission. The ATA is an integrated single-phase mechanically pumped fluid-loop (MPFL) thermal control system developed for high-power small-satellite applications. The ATA is constructed using 3D Ultrasonic Additive Manufacturing to co-fabricate the internal thermal transport channels and structural members, enabling direct integration of heat exchangers and fluid pathways within primary spacecraft components. The resulting architecture reduces mechanical interfaces, improves thermal transfer, and …

Development Of Wavelength-Division-Multiplexed All-Optical Relays For Low-Earth Orbit Free-Space Optical Communication Networks, Travis Jones, Justin Cook, Chris Krush, Doruk Engin, Keith G. Petrillo

Small Satellite Conference

In this work, we designed, built, and tested an all-optical relay amplifier to enable a space-based all-optical backbone for laser communications networks. The design sought to optimize links for LEO-based networks incorporating appropriate span lengths and optical terminal specifications. We incorporate an add-drop multiplexer for rerouting signals and designed the system to be flexible over span lengths with a nominal range of 1,800 km. We performed several tests of the nominally 60 dB gain amplifier to assess link dynamics unique to free space optical communications (FSOC) including the impact of pointing jitter, nonlinearities, gain flattening, and wide-band filters on an …

Delay/ Disruption Tolerant Networking In Cislunar Space, Sara Garcia-Beech, Rebecca Besser, Elizabeth Geist, Theresa Beech, Mike Palsson, Krishnan Narayanan, Ben Anderson

Small Satellite Conference

DTN (Delay/Disruption Tolerant Networking) is at foundation of NASA's LunaNet architecture, which will enable the robust communications, navigation, and networking capabilities needed to establish a long-term presence on the Moon. DTN is a network architecture composed of several different protocols that are designed to provide internetworking functionality and standardized multi-hop, end-to-end data delivery in highly stressed environments that are not optimal for traditional Internet Protocols. Bundle Protocol (BP) version 7, a store-and-forward protocol intended to run at the application layer on top of convergence layer protocols, provides the key delay tolerance functionality of DTN and is designed to handle intermittent …

Event-Driven Spacecraft Operations Demonstrated On Mms, Miles Bengtson, Alexander Barrie, Joseph Patton, Liam Greenlee, Paul Wood, Marcus Piquette, Russell Bjella, Matthew Chang, Joshua Paul

Small Satellite Conference

Operations engineers face the challenging task of capturing high-value science data while maintaining spacecraft health and functionality and responding to a dynamic space environment using limited information. This task is becoming increasingly complex as missions involve increasingly large numbers of spacecraft, target more elusive science signatures, and operate under growing budget and staffing constraints. Conventional pre-programmed time-sequence commands become increasingly burdensome for multi-spacecraft missions and are fundamentally incapable of reacting to rare, transient science events in real time.

To address this challenge, we have developed MEDOS: the Module for Event-Driven Operations of Spacecraft. Unlike machine learning and neural-network approaches, MEDOS …