Digital Commons Network^™

A Ground System Framework For Operating Satellites In Very Low Earth Orbit, Kashyapa Naren Athreyas, Bryden Cho, Xiaohua Zhang, Wee Seng Lim

Small Satellite Conference

In the space industry, the space-segment and ground-segment work in tandem to effectively and safely control satellites, execute its intended missions, and obtain meaningful data. In recent years, the space industry has been exploring Very Low Earth Orbit (VLEO) for the following advantages: (a) reduced satellite traffic, (b) increased revisit frequency, (c) shorter communication distances, and (d) closer Earth observation points. However, the exponential increase in atmospheric density and gravitational forces, combined with shorter operational response times to critical events, poses significant challenges for satellite operations. While satellite design should ensure appropriate system sizing and requirements to address these issues …

The Development Of Dwts (Doppler Wind Temperature Sounder) Climatology Missions For Earth And Mars, Marcus S. Murbach, Alejandro Salas, Arwen Davé, Malachi Mooney-Rivkin, Avery Brock, Kwabena Boateng, Ali Kashani, Larry Gordley, Benjamin Marshall, Joe Gubeli, Amanda Cook, Donald Banfield, Anthony Colaprete

Small Satellite Conference

The Doppler Wind and Temperature Sounder instrument (DWTS) is a unique atmospheric instrument being developed by Global Atmospheric Technologies (GATS), NASA and NOAA. Invented by Larry Gordley/GATS, it is a mid-wave infrared camera paired with a nitrous oxide (NO) cell, which acts as a spectral filter. Wind velocities and kinetic temperatures in the stratosphere and lower thermosphere are extracted by measuring the induced Doppler shift and Doppler broadening of emissions as they pass through the DWTS field of view. Eventually, the use of 3 gas cells(N2O, CO2) would complete the complement such that 20-200km during the day or night could …

Using A Software-Defined Radio Ground Station For A Small Satellite Mission, Simon Gläsner, Victoria Koßack, Mario-Rafael Ionian, Enrico Stoll, Tom Baumann

Small Satellite Conference

In January 2025, InnoCube, a 3U CubeSat was launched with the Transporter-12 mission, becoming the 31st academic satellite of TU Berlin. The technology demonstration mission is the first one at TU Berlin which uses software-defined radio to operate the satellite in the amateur UHF band. The ground station is based on software-defined radio, which has been a vital part of the development of the communication system of InnoCube. Integration into the ground segment is a logical step in the test-as-you-fly philosophy of the mission. The ground segment consists of a SDR which is paired to a power amplifier which includes …

Laser Crosslink Experiment: Post-Mission Review, Sean Stanko, Dan Frey, Jose Ruvalcaba, Sean Burk, Damian Klaren, Dmitriy Obukhov, Barry Tidmore, Jason Bousquet, David Wayne, Nathan Barnwell, Galen Cauble, Kevin Book, Ben Laxton, Grant Webster, Stan Volchenok, David Sadowski, David Palmer

Small Satellite Conference

The Laser Crosslink Experiment (LaCE) was a Low Earth Orbit (LEO) microsatellite mission that flew between March 4, 2024, and May 18, 2025. LaCE was a two-CubeSat, multi-payload mission developed by Naval Information Warfare Center Pacific (NIWC). Its major payloads included the CACI Skylight laser communication terminal, the ELROI optical beacon, the Vulcan CSR payload radio, and a newly developed NIWC Tracking, Telemetry, and Command (TT&C) ground operations center. Additionally, LaCE led to the development of the Stratospheric Optical Link Demonstration (SOLD) high-altitude balloon experiment, a companion mission which demonstrated the Skylight terminal in the stratosphere as a risk reduction …

Apophis Cratering Experiment Mission Concept, Ethan Kayser, Tyler Presser, Cristyn Merry, Matthew Givens, Kevin Walsh, Viliam Klein

Small Satellite Conference

Apophis is set to become one of the most extensively studied asteroids in history thanks to the detailed observation campaign of OSIRIS-APEX during its 2029 and 2030 extended mission to the near-Earth object, alongside Ramses which is expected to launch in 2028. To supplement those missions, we propose the Apophis Cratering Experiment (ACE), an impactor mission that leverages OSIRIS-APEX or Ramses as a dedicated observer, during and after the collision, to maximize scientific return at a low cost. In addition to providing significant science return, the mission offers a low-cost opportunity to demonstrate novel SmallSat technologies in deep …

The Move Towards A Modular Spacecraft: Design And Manufacture Of Rf Components Using Additive Manufacturing, Rupesh Chudasama, Benjamin Falkner, Evangelos Mellios, Hossein Eskandari

Small Satellite Conference

Waveguides are critical components for communicating with satellites. Traditional waveguides consist of two parts and are relatively simple in geometry and require multiple steps and fasteners for assembly which add additional weight and the extended delivery times. Our approach is to use Additive Manufacturing (AM) and its design freedoms to produce a lighter, more compact, and printable version of a waveguide. The waveguide will undergo electrical testing to understand the performance of the 3D printed waveguide against the simulation.

Optimizing Ground Station Communications Using Multiple Spacecraft Per Aperture In A Ground Segment As A Service Framework, Stefan Vlad Tudor, Giovanni Zanotti

Small Satellite Conference

The increasing deployment of satellite clusters in Low Earth Orbit (LEO) presents new challenges and opportunities for satellite communications, particularly from a Ground Segment perspective. This paper investigates efficient management of multiple ground contacts, in the Ground Segment as a Service context, by leveraging on Multiple Spacecraft Per Aperture (MSPA) technique to maximize connectivity by sharing ground resources to multiple satellites simultaneously.

MSPA is particularly valuable for handling multiple spacecraft in close proximity, such as during the Launch and Early Orbit Phase (LEOP) of rideshare missions, all being supported by same ground segment infrastructure. By enabling simultaneous downlinks through a …

Advancing Real-Time Gnss Data Transmission And Education Through Atak Integration At Cosmiac, Chad Rathbun, Craig Kief, Luis Hernandez, Rachel Hock-Mysliwiec, Michael Starks

Small Satellite Conference

This study showcases COSMIAC at the University of New Mexico (UNM), a leading center for configurable space microsystems and aerospace applications, as it integrates cutting-edge technologies to advance secure and efficient communication systems. Under the AFRL RAPID program, COSMIAC tested a novel architecture combining Azure Orbital Cloud Access (AOCA), the Azure Stack Edge Mini Rugged device, and SpaceX’s Starlink satellite constellation to transmit real-time Global Navigation Satellite System (GNSS) data. The project also leveraged the Android Tactical Assault Kit (ATAK), a geospatial situational awareness tool, to demonstrate the operational utility of advanced data delivery and visualization systems. The results inform …

Ai-Driven Mission-Critical Software Optimization For Small Satellites: Integrating An Automated Testing Framework, Vishnupriya S. Devarajulu

Small Satellite Conference

Small satellites (SmallSats) have revolutionized our modern digital infrastructure, such as Earth observation, navigation, real-time communications, and deep space exploration, due to their composable design, effectively reduced cost, and accelerated development cycles. However, SmallSat software must function autonomously, often under limited bandwidth, processing power, and computing resources. Pre-launch techniques such as Hardware-in-the-Loop (HIL), Software-in-the-Loop (SIL) and Unit testing are generally used, but often insufficient to detect errors, timing anomalies, fault propagation, or further telemetry-based degradations. This paper presents a Python-based validation framework influenced by recent testbeds like EIRSAT-1, ITASAT-2, and NOS3, integrating telemetry simulation, synthetic fault injection, resource logging, anomaly …

Autonomous Dual Interchangeable Robotic Arms For In-Space Servicing, Assembly, And Manufacturing, Jonathan Tindall, Michael Daher, Arin Churi, Jake Piccirillo, Anais Mera-Sarnelli, George Serra, Zach Merly, Andrew Dishchuk, Michael Madden, Christian Szczezniak

Small Satellite Conference

The expansion of Low Earth Orbit (LEO) satellite constellations highlights the critical need for In-Space Servicing, Assembly, and Manufacturing (ISAM) to perform novel orbital missions that reduces launch and operating costs and extends mission lifespans. Existing space robotic systems are too expensive, large, and specialized for many ISAM applications in LEO. A small-scale twin robotic arm system that features interchangeable end effectors enhances future ISAM mission capabilities. This robotic arm system leverages smaller, low-cost, arms to perform precise autonomous operations, including satellite repair, repositioning, and recovery. Initial designs and analysis show the arms to be 62% smaller in length and …

Building Europe’S First Isam Facility – From Concept To Delivery In 12 Months, Mark Heelis, Dimitris Xydas, Alex Goodhand, Jeremy Hadall, Elanor Barber, Rupesh Chudasama, Olivia Markham, Michael Curtis-Rouse

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Chantsat-1 Ground Station Planning, Design And Installation - Experiences Gained, Ian Hewitt, Jean French, George Hitt

Small Satellite Conference

Planning, designing, and implementing the ground station for ChantSat-1, Coastal Carolina University’s first small sat mission program, was the first major milestone of the University’s space program. CCU’s ChantSat-1 ground station team presents the experiences gained during the process from inception to completion of the ground station at a liberal arts public University in the southeastern United States with approximately 11,000 students. By sharing both our challenges and successes, our goal is to support others by providing experiences gained in the process.

Chantsat-1: A First-Time University's Experience In Small Satellite Development, George Hitt, Jean French, Juliana Harding, Ian Hewitt, Louis Keiner, Michael Woodle

Small Satellite Conference

ChantSat-1, Coastal Carolina University (CCU) High Altitude Nadir-pointing Satellite-1, is the first smallsat mission envisioned by our primarily undergraduate university. Capacity development to support mission planning over 18 months has integrated a range of interdisciplinary stakeholders while capturing the attention and imagination of students. The mission’s primary payload will be a multispectral camera for remote sensing of South Carolina’s coastal blackwater rivers, estuaries, and adjacent ocean shelf waters. The resulting coastal habitat mosaic supports ecologically important food webs and related economic and cultural engines of regional growth, while being uniquely vulnerable to the combination of natural episodic climate-related events combined …

Development Status Of Flight Model Of Arica-2, Kazumasa Hiroshi, Takanori Sakamoto, Motoko Serino, Keiju Asano, Chisaki Iwanaga, Yoshihiro Takagi, Shion Nojima, Hayato Mabuchi, Shuntaro Morikawa, Rento Okita, Satoshi Moriayama, Teruaki Enoto

Small Satellite Conference

ARICA-2 (AGU Remote Innovative CubeSat Alert system -2) is a 2U CubeSat developed in AGU (Aoyama Gakuin University) in JAPAN. ARICA-2 was selected as the as the JAXA Innovative Satellite Technology Demonstration-4 and is scheduled for launch in Japanese fiscal year 2025. The mission objective of this satellite is to demonstrate the real-time alert system of sudden astronomical phenomena, such as gamma-ray bursts (GRBs). Observation of GRBs is challenging because it is difficult to predict location and time of occurrences and its extremely short duration. So, it is necessary to alert immediately for tracing observations of GRBs from the other …

Efficiency Starts With Lifecycle Planning, Management, And Right-Sizing Process, Brian Simms

Small Satellite Conference

When a program starts, there's a tendency for management or leadership to want to get things moving, to get going, to start doing things. It makes a lot of sense to push forward, but only if everybody understands what "doing things" means. A lot of the time, there's a lack of initial process or clarity about where in a specific process we're starting. Sometimes goals, expectations, and processes don’t reach every member of the team.

In a time when efficiency is being leveraged as a weapon to defund existing efforts, all programs are immediately operating at risk. Programs desperately require …

Foresail-1 Prime 3u Science Cubesat, Jaan Praks, Petri Niemelä, Marius Anger, Kiril Cheremetiev, Topi Räty, Minna Palmroth, Emilia Kilpua, Pekka Janhunen, Rami Vainio

Small Satellite Conference

The Foresail-1 Prime is a satellite mission developed by Aalto University in association with the Finnish Centre of Excellence in Research of Sustainable Space (FORESAIL). The mission carries scientific payloads such as the Particle Telescope (PATE), Plasma Brake Experiment (PB), magnetometer MATTI and features fully in-house developed subsystems. This is the fourth satellite, developed by Aalto University, building on heritage of Aalto-1, Aalto-2 and Foresail-1 satellites.

Experimental Validation Of Omnidirectional Interferometry For Space-Based Radio Source Localization, Hisatoshi Kimura, Yosuke Tanabe, Tsukasa Funane, Makoto Ito, Yasuyuki Miyazaki, Satoshi Ikari, Shinichi Nakasuka, Koichi Watanabe

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Modular Payload Connectivity For Rapid Integration And Testing, Sam Feldman, Noah Gladden, Rahul Rughani, Dave Barnhart

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Next-Generation Earth Observation: Agile Satellites With Cmg Cluster For Enhanced Coverage, Andrea Coco, Simon Debois

Small Satellite Conference

The rapid growth of Earth observation demands cost-effective strategies, such as integrating COTS components and accelerating deployment. A key factor in mission efficiency is spacecraft agility, which enables faster reorientation, improved target tracking, and optimized data collection. A game-changing advancement is the revival of Control Moment Gyroscopes (CMGs) as cost-effective, high-performance actuators. Once constrained by high costs, recent manufacturing innovations and new providers have made CMGs more accessible. With superior torque efficiency and capability, CMGs greatly enhance agility, enabling faster reorientation and improved data collection compared to conventional reaction wheels. This paper presents a comparative case study demonstrating the advantages …

Orbital Decay Analysis Of Uae Nanosatellites In Low Earth Orbit, Bassam Alfeeli

Small Satellite Conference

Given the continuous efforts in the United Arab Emirates (UAE) to develop its local capabilities in space technology through the deployment of nanosatellites (cubesats) in Low Earth Orbit (LEO), understanding cubesats orbital dynamics and decay patterns is crucial for both future mission planning and space debris management. This study investigates the orbital decay characteristics of cubesats deployed by the UAE in LEO. We analyzed the orbital decay rates of seven UAE cubesats namely Nayif-1, Mysat-1, Meznsat, QMR-KWT, Ghalib, Dhabisat, and Light-1 by examining observational data, orbital parameters, and environmental factors. The results offer insights into the effectiveness of current satellite …

Orbitcare: A Universal Autonomous In-Orbit Platform For Manufacturing, Servicing, And Debris Mitigation, Rohan Chandratre, Vishish Behera, Anushree Manwatkar, Aruma Kushwaha, Sneha Gayen

Small Satellite Conference

OrbitCare is a proposed orbital infrastructure enabling scalable, sustainable, and cost-effective in-space servicing, manufacturing, and assembly through a modular system architecture comprising an Orbital Manufacturing Hub (OMH) and a fleet of free-flying WorkSat servicing satellites, all integrated via a standardized Servicing Interface Standard (SIS). This paper presents the technical architecture, subsystem design, trade studies, use cases, and development roadmap for OrbitCare. The motivation stems from the current lack of persistent infrastructure in orbit, which renders satellites single-use assets with limited repair or upgrade capabilities. OrbitCare addresses this by combining a permanent hub with reusable robotic satellites to extend spacecraft lifespans, …

Small Satellites, Big Impact: Advancing Space Innovation From Earth To Orbit With The Catapult’S Isam Test Facility, Dimitris Xydas, Oliver Knappett, Lewis Gray, Alex Goodhand, Jeremy Hadall, Michael Curtis-Rouse

Small Satellite Conference

The In-orbit Servicing Assembly & Manufacturing (ISAM) Test Facility at Westcott, UK is a testbed providing realistic environmental conditions for orbital operations here on Earth, with the primary objective of accelerating the readiness level of emerging ISAM technologies and reducing the time to market for commercial space systems. As a result of continuous feedback from campaigns, the Facility has seen recent upgrades to both infrastructure and capabilities, which has created a unique operational environment that acts as an enabler for space activities in the UK and internationally. Moreover, as a constantly evolving system, it is uniquely positioned to adapt to …

The Potential Of Small Optical Isolators For Leo Satellite Equipment, Tomoaki Toriya, Shuto Goryo, Masaki Ogura, Fumiaki Shiotsu, Toshihisa Okubo, Takashi Kato

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

A Small-Satellite On-Orbit Optical And Thermal Calibrator, Paul D. Fucile

Small Satellite Conference

Imaging payload sensor calibrations are typically performed under laboratory conditions prior to launch and then routinely while on-orbit by using ground or astronomical based reference sources. With a trend towards autonomous operations, many machine-learning algorithms would benefit from having on-demand calibration across multiple detectors to better enable capabilities, for example using long wave infrared observations to identify and distinguish clouds from snow and ice. This subsequently would allow satellites to identify clouds confidently onboard, and downlink well defined clear images.

Presented are two technologies that provide a method for the direct on-orbit calibration of optical and thermal cameras used in …

Techniques For Optimizing Swap-C Through Multi-Phase Clock Distribution, Abigail Eberts

Small Satellite Conference

Multi-phase power is important to design highly efficient solutions for next-generation space avionics systems, but noise, current sharing accuracy and beat pulses can all contribute to the complexity of a power system's design. The latest FPGAs and ACAPs have very specific DC and AC regulation tolerances, so it can be difficult to manage power while considering size, efficiency, reliability and cost.

This poster will demonstrate methods to scale and manage multi-phase power systems through the inclusion of power management-specific clock distribution ICs and show how they can be used to implement a variety of solutions that balance efficiency and accuracy …

Ronald E. Mcnair Scholars Program Profiles And Abstracts 2025, Mcnair Scholars Program

McNair Symposium

This publication provides research abstracts and biographies of 2025 McNair scholars and their mentors.

Modernizing Smallsat Mission Operations: Integrating Ai-Driven Optimization With Cloud-Native Control Systems, David Besson, Dax Garner

Small Satellite Conference

As the space industry experiences unprecedented growth in SmallSat constellation deployments, traditional mission control approaches face significant scalability and efficiency challenges. This paper presents a novel framework that integrates three cutting-edge technologies to revolutionize satellite mission operations: Cognitive Space’s CNTIENT.Optimize AI-powered decision engine, Yamcs open-source mission control software, and the Amazon Web Services (AWS) Cloud Mission Operations Center (CMOC) solution. As a representative simulation benchmark, the paper demonstrates the framework’s capabilities through mission simulations of the Cyclone Global Navigation Satellite System (CYGNSS) SmallSat constellation. The integration leverages CNTIENT.Optimize’s advanced AI algorithms to automate complex scheduling decisions across proliferating homogenous or …

Arizona Dust: Students Advancing Climate Science With Cubesat Technology, Haile Brown, Theodore Courtois, Alyssa Armstrong, Abraham Phillips, Mckayla Morgan, Isabella O'Brien, Aaron Wall, Harrison Constance

Small Satellite Conference

ARIZONA DUST (Arid Region Infrared Zone Observation of Notable Arizona Desert Urban Storms and Temperatures) is a student-led mission team of 25 out of Arizona State University with the goal to understand how Earth’s climate is evolving and why. The 6U CubeSat ‘Dusty’ will orbit at a 400 km altitude in a non-sun synchronous orbit with a 40^° inclination designed to pass over Arizona (as well as Australia). The mission is designed to study monsoon and dust storms to enhance understanding of their effects on temperature as they relate to global climate change. With the orbital path also crossing …

Afrl Validated Principles And Building Blocks Of Ground-Based Ops Automation, Tyler De Caussin, Jarred Langhals, Brandon Shirley, Lee Jasper

Small Satellite Conference

Over the past decade, AFRL's Small Satellite Portfolio (SSP) and Ops Cadre (RVES) branches have been operating small satellites with different bus providers to support diverse mission needs. Because the bus, payload and experimentation differ for every mission, and the ground segment has had the challenge of supporting the varying needs on a mission-by-mission basis. AFRL has been working to improve efficiency with which the ground segment supports those varying needs. One major emphasis has been on learning how to automate operations of such different missions. In an effort to standardize mission automation within the operations center, AFRL has developed …

Terp Raptor: A University-Led Smallsat Flyby Mission To Investigate Asteroid Apophis, Adrienne Rudolph, Sean Phillips, Chinthan Prasad, Kruti Bhingradiya, Rahul Vishnoi, Cameron Storey, Brent Barbee, Mary Bowden, David Akin, Jarred Young, Paul Bernhardt, Yunghsin Chen

Small Satellite Conference

The ~350-meter diameter Potentially Hazardous Asteroid (PHA) designated 99942 Apophis 2004 MN₄ will make a historic close approach of Earth on April 13th, 2029, passing within ~31,634 km of Earth’s surface, closer than our geosynchronous satellites. Suggested to be a 1 in 7500-year event, this is an extraordinarily unique opportunity for collecting data on an Apophis-sized asteroid experiencing the effects of Earth’s gravitational field. Our Terrapin Engineered Rideshare Probe for Rapid-response asteroid Apophis Profiling, Tracking, Observing, and Reconnaissance (TERP RAPTOR) is a low-cost, Earth-orbiting mission concept in which a 12U CubeSat designed and built by University of Maryland students …