San Diego Section of IEEE Invited Talk Intersects ORI’s Antenna Work

In Pursuit of Low-Cost, Multifunctional, and Electrical Small Antennas for Microwave and Millimeter-Wave Communications

Prof. Ashwin K. Iyer
University of Alberta

20 July 2026
SDSU EIS-320 Conference Room
1500 – 1600

Attendance of 11 including speaker.

Dr. Satish Sharma (SDSU, and the organizer of the talk) introduced Dr. Iyer, describing his successful lab and shared connections with warmth and enthusiasm.

Dr. Iyer is fortunate to have the room to broadly explore antenna design topics in miniaturized microwave antennas. It was clearly evident from the presentation that his leadership is making an ongoing and enduring impact.

The talk covered many of the projects under consideration in his research group at the University of Alberta, located in Edmonton, the capital of the province. Located east of the Rockies, Edmonton is the most northern city in Canada with population of more than a million people and it serves as Canada’s primary logistical interface to the Arctic and boasts the continent’s largest stretch of continuous urban parkland. Research supporting tactical operations in the Arctic was a thread woven throughout the presentation.

The University of Alberta has over 46,000 students distributed among 18 faculties and generates 600 million in sponsored research revenue per year. It has a major open-access nanoFAB, which is free for use by students and open to industry to use as well. The ECE department has 60 faculty and is one of the largest ECE departments in Canada.

After this brief introduction, we had a pop quiz! Dr. Iyer showed two photos of people and asked “Who are they?” They were the bachelor’s graduation photos of George Sinclair, and Edward Jordan. George studied slot arrays, radar scattering, scale modeling. Edward researched antennas and radar, but is recognized for significant contributions to antenna education. Both were affected by their PhD advisor being absorbed by the US Signal Corps during WWII.

These two engineering researchers were pioneers in Canada, establishing antenna labs and attracting lots of researchers. Classical antenna science moved forward due to their efforts, and both Dr. Sharma and Dr. Iyer have connections their work.

The primary research theme of the lab is very low profile, weight, power, and cost antennas and microwave devices. “Low SWaPC” The lab focus includes the synthesis and modeling of denied EM environments. Antennas, sensors, meta-material devices for GPA, GPR, wires communications, security defense, and oil and gas are all considered. Defense work is a large part of the lab focus.

This means that the research concerns lots of sensors, antenna platforms, integrated platforms, zero-power biometric sensing, ad-hoc networks, meta-surfaces, signature management, and radar cross section. The lab partners with a variety of companies and organizations that those of us in the San Diego Section would be very familiar with.

The motivation is to innovate and refine electrically small antennas, meta-material-based antennas, and small antennas.

Challenges? There are clear challenges to this type of work. There are fundamental limits on bandwidth, quality factor, and gain. Matching impedances to the components and the environment is one of the most difficult challenges for very small antenna designs.

In order to get power radiated from even a very small antenna, you need a matching network. That matching network might be very bulky compared to the miniaturized antenna. If you do manage to get power into the antenna, the bandwidth ends up being small, because of losses exacerbated in the antenna. Small structures are difficult. Radiation efficiency is strongly reduced.

Dr. Iyer introduced an “Inherently Matched” electrically small folded dipole. Usually a half wavelength is the operating size/length of a dipole antenna. The resonance point was clearly shown on an impedance vs. length graph. Moving the resonance down, so that we get a smaller length, is the goal.

We reviewed inherent matching technique for Frequency Division Duplex Electrically Small Antennas (FDD ESAs). Dr. Iyer explained that the printed folded dipole with lumped L and C loading was used with positive results. This is a miniaturized planar folded dipole.

An Illuminating Contrast to ORI Work

A fully printed folded dipole looks very similar on the surface to Open Research Institute’s HF Dumbbell antenna, which uses a meander dipole structure at HF to dramatically reduce the physical size of a wire antenna while delivering high radiation resistance. Meander dipole miniaturization and tuning of planar printed dipole antennas clearly achieves high radiation efficiency while reducing size. Essentially, this is about min-maxing radiation efficiency vs. size, using meanders.

In traditional antenna miniaturization, engineers add physical, discrete components, such as a physical coil (inductor) or a physical capacitor (ceramic chip) to force a short antenna to resonate.

An HF or shortwave meander dipole antenna relies entirely on distributed (or parasitic) self-inductance and self-capacitance created inherently by its structural shape. The meander doesn’t radiate, but the remaining straight section of wire certainly does. At HF, the meander section is treated primarily as a delay line or a slow-wave structure rather than the primary source of the radio waves.

For the microwave structures that Dr. Iyer’s research group considers, the meander sections do radiate at microwave, but they do so in a highly asymmetric way that defines the polarization of the antenna.

Dr. Iyer’s Microwave Meander is a 2D structure on a dielectric substrate, perfect for integrating into miniaturized products. ORI’s HF antenna is a 2D Meander wrapped around a cylinder in order to create a sturdy structure that can be put up on a mast to get it high up enough to go on the air at the minimum HF antenna size.

Dr. Iyer’s microwave meanders act as the actual distributed radiator while compressing the physical length. At HF, ORI’s Dumbbell antenna acts as a non-radiating delay line to slow the wave speed down. Waves exit Dr. Iyer’s antennas broadly, including the meander section. At HF, ORI’s antennas see the waves exit in the straight wire sections, and not in the meander sections much at all.

At microwave frequencies, the tuning burden is on discrete components, instead of relying upon the physical meander structure of the antenna. This means that the meander is freed up to act purely as an efficient, compact, distributed radiator, allowing the antenna to maintain high radiation efficiency despite being much smaller than a conventional dipole.

The next example was a miniaturized RFID tag. Unbalanced currents on the feed, for small antennas, mean that the feed might end up radiating more than the antenna. To solve this clear and present danger to the utility of the antenna. Dr. Iyer’s group puts the RFID chip directly on the antenna. In other words, there is a conjugate match from the RFID chip directly to the antenna, in order to have the input impedance of the actual RFID chip be the target of the antenna match. There is no matching network, and therefore, no feed loss. Looking at the received signal strength, the quality of this match approach was confirmed. Essentially, this is abandoning the conviction that a 50 Ohm matching network must be between the RF signal output of the RFID chip, and the input electrical point of the antenna structure. The antenna matches whatever the RFID chip can produce, and then translates that to a “match” with free space.

The next example was an RFID-based temperature sensor, designed for free space or on-body applications. The on-board capacitor detunes antenna and temperature is detected. This ultra-miniature antenna has resonance frequency shifts across the RFID band that are correlated with temperature. The channel moves as the temperature changes the capacitor. This detunes the antenna. The 12 by 18 mm footprint is very small. The antenna geometry is designed for a conjugate match to the RFID chip impedance. The sensor radiates on the body, on the fingertips, and is designed to detect frostbite.

We then considered a concrete curing example. What if we included sensors in concrete? We would embed sensors for tracking the temperature and physical status. We can determine from the temperature profile how well a concrete structure has cured. The resonances are very narrow, and a fracture in the vicinity will shift the resonance. If the sensors last, then you can find failures over time.

Side note, Canada has an over the horizon radar project going on (30 feet high, 60 feet separation, over football field in width).

Dr. Iyer explained that traditionally, it has been mostly an ad-hoc process to miniaturize an antenna. He wanted to systematize the process, and he feels that they are making strong and consistent progress on this question.

Dr. Iyer changed gears from case studies and research projects to frame the Chu Limit, and what all this work means in terms of basic antenna theory. Antennas have a certain bandwidth capacity and quality factor. How low can it go for a certain size? This what the Chu limit addresses. The orginal research dates back to 1948 and involves circuit ladder networks, spherical wave expansions, and was done rigorously for the first few multipole orders, due to how grueling the computations were at the time. In 1964 Collins and Rothschild used field integration to confirm the Chu limit. However, Collins and Rothschild bypassed Chu’s circuit equivalents entirely when they did this. They calculated the stored energy by integrating the electromagnetic fields directly through space. While they arrived at values that mathematically matched Chu’s lower orders, a subtle and frustrating problem emerged in basic antenna theory. There was no universal, formal proof proving that Chu’s discrete equivalent circuit approach and Collins/Rothschild’s continuous field integration approach would always reconcile perfectly for an infinite number of higher-order multipole modes. It remained an unresolved, tricky gap in the fundamental literature.

So, Dr. Iyer’s lab united the theories and proved it with mathematical induction. What does this mean? The successfully bridged the two independent theories, which is a major contribution to the field. They proved that Chu’s ladder networks and the field integration models are dual expressions of the exact same physical reality across all arbitrary multipole orders, not just the first few. Mathematical induction really shines in this exact case, by taking a few successful solid results and extrapolating (correctly) to some larger or even infinite range of results.

By shifting the conversation from “how do we load this specific meander in this specific application” to “let’s mathematically unite the fundamental bounds of stored energy,” the research provides all of us engineers with an exact framework to evaluate exactly how close a highly miniaturized design (like the printed or cylindrical antennas discussed earlier) is to the absolute boundaries allowed by physics. This is delightful.

How does Dr. Iyer’s lab design optimal spherical miniature antennas? The optical geometry for spherical helical antennas can be predicted. Theory and results agreed for the structures that the lab tackled.

The next project was the leveraging of RFID to test small antennas. An achieved Ka, which is the dimensionless electrical size parameter, of 0.2 at 900 MHz, was presented and explained. Anything under 0.5 Ka is considered an electrically small antenna, so this is not a borderline result.

The reported Q of 198 or about 1.5x EP lower bound was then discussed. The quality factor Q inversely defines the antenna’s bandwidth. Because the antenna is tiny, its Q naturally skyrockets. The “EP lower bound” refers to the Elliptically Polarized lower bound. This is a stricter fundamental limit derived from spherical wave expansions. Achieving a Q of 198, which is only 1.5 times the absolute physical limit allowed by physics for that size, is an extraordinary design achievement indicating maximum possible bandwidth.

The particular antenna in this part of the presentation looks like a sake barrel with bifilar spherical helix arrangement wrapped around it. There is no feed network, as the RFID chip is directly connected to the antenna. Uniting the feed and the antenna is a key design pattern of the work in the lab.

This is one of several designs from Dr. Iyer’s lab where the traditional dipole arms are wrapped into a 3D spherical shell to maximize the utilization of the “Chu sphere” volume. “Bifilar” simply means it uses two symmetrically wrapped helical wire arms.

The slide presentation concluded and we went to Q&A.

Q: normally what is the level of power or gain that you usually get?
A: Close to the 1.5 dB limit. Which is much better than -13 dB that a lot of miniaturization ends up with. Usually it’s a horrible compromise between power and size.

Q: Can we use dispersion engineering to get multifunctional antennas and circuits?
A: Yes.

Dr. Iyer described how they designed a method of moments (MTM) based structure that is compact, uniplanar, fully printable, and included the full design procedure. This is a meta-material based electromagnetic bandgap structure MTM-EBG.

Coupled mode theory is used to produce a controllable bandgap. With a microstrip line, if you have two conductors, you have one mode.

So we can slot this structure and we can then produce something with, say, 4 conductors and therefore 3 modes. All TEM therefore they don’t couple. So, to force them to couple, we can make gaps and connect the conductors.

We load some conductors with capacitors and some with inductors. Phase might move backwards but the power always moves forwards.

The bandgap is created with coupled-mode dispersion. It can be printed. Printed gaps, printed conductors. Can you use this to build a multi-band antenna in one layer? Yes indeed. We “create two resonances for the price of one.”

Good operation was observed in both bands. Dual band and dual polarized patches were prototyped, at 3.6 Ghz and 5.8 GHz. They were fabricated and measured. They came in 1-1.4 dB lower than an equivalent patch antenna, but were much smaller.

Next, GPS/GNSS Antenna were shown, using a multi-layer MTM-EBG structure for the antenna design. This is a stacked patch antenna. Dr. Iyer’s lab collapsed it to a single patch, dual band at L1 and L2/L5. Solid PLA is the substrate. Extremely accurate due to the collapsed structure, on the order of 2mm resolution. Calian is the company that the lab is collaborating with, and commercialization of this antenna is expected in the next little while.

Dr. Iyer’s discussed the University of Alberta student cubesat project AlberatSat (launched twice). The project had turnstile rod antennas that mechanically deployed, but on the second launch they failed to deploy. Dr. Iyer’s lab proposed a flat antenna that has no moving mechanical parts? 437.5 MHz and S-band, patch antenna, instead of the turnstile rods.

Dual-band patch antenna design is 150mm by 86 by 6.35mm. It is mounted on the Nadir face, faces earth, and looks like it meets all their specs and will fly.

Drawbacks? It’s heavy. It’s like about a pound. To avoid the point of failure, the extra weight may be worth it. With and without the rails, with and without the cubesat package, was designed to be on the satellite.

Next up was a 20/30 GHz dual band. There are interior and exterior regions of the antenna. The gap sizes are 50 microns. This means very precise construction is required. Key aspect of this design is the ability to vary the polarizations and combinations of polarizations. This was achieved with chamfering the corners. It does produce the desired radiation characteristics. Physical prototypes showed port isolation larger than 25 dB.

How can we apply the MTM-EBG in other areas? Compact filters. Double-stub tuners. Stub matching networks. The lab is controlling the flow of current through the EBG regions. Uniplanar, three bands of matching. Capacitor and inductor going to ground, frequency dependent load, and designed for that load. Single port, complex impedance, chosen arbitrarily, so it can be redesigned for pretty much any load. Can be designed for three independent frequencies.

MTM-EBG based mechanically tunable filters were presented. Absolute bandwidth changes lowers with target frequency. But, what if we want consistent bandwidth? Filter is designed to maintain constant absolute bandwidth. Independently tune the three unit cells in the construction, and the problem is successfully addressed.

Next: Transmission line crossover. What about phased arrays? You have one PCB layer, but you want to operate in two different frequency bands. This is a challenging problem. Dr. Iyer showed a compact microwave filter for operation at 2.4 and 5.8 GHz. Like two train tracks that cross over each other.

Next was RFID-based real-time battery level monitoring, with a dual band antenna and diplexer system. Energy harvested in the field from 2.4 GHz enables communications over 915 MHz. Harvest to a battery, varactor across the battery. Modulate the impedance, backscatter communicate the battery level. Battery level goes up, varactor capacitance goes up, and the phase changes, and RFID backscatter indicates the voltage level on the battery. (see the OJAP special issue on antenna-enabled sensors and systems for more information about this particular design)

Dispersion Engineering is Fun

For meta-surfaces, can we use single sheets of flexible circuits to do wave front engineering? Yes we can. Waveguides and radomes are where this shows up.

We have flexible printed meander dipoles and we wrap this around a cylinder to where the pattern repeats.

This has a particular and interesting application in MRIs, where we change the frequency without requiring steep increases in the Tesla required of the magnets. You can fill the entire MRI with a dielectric, but those pesky patients kind of get in the way. The result of Dr. Iyer’s work is reduced risk of burns and better quality results without requiring big increases in Tesla.

Another case study is sectorized antennas for cellular phones. These sectors have seams. The seams are not perfect. There’s different ways to address this. Overlap the sectors, or rework the antenna, or use meta surfaces in radomes in order to change the pattern and reduce the impact of the seams. Placed over the antenna array, the material modifies the gain pattern. The dual use of this is signature management, to change the characteristics of an antenna in the field to avoid detection.

Q: What is the size of the GPS Antenna?
A: 80mm or so

Q: What do you use for antenna modeling?
A: Mainly HFSS, FICO, CST

Dr. Iyer closes with describing and emphasizing the value of a teacher and teaching in general. Doing things with a certain level of integrity, whether you are teaching in the literal sense, or doing something for the benefit of others, the quality and values of your advisor is key. Dr. Satish Sharma highlighted Dr. Iyer’s quality of work and teaching excellence.

Dr. Satish explained that SDSU has offered a lot of master’s level work to students, traditionally. Over the years, it’s grown and developed into better research environment for PhD work. Now there is a joint PhD program with UCSD, for example. However, some students want to just get the degree and get out. That is ok, because they are on a self-assigned mission, or see a need that needs to be filled somewhere in the world and they are drawn to it. Some students are at University to learn and study deeply, and make a real difference within the research lab or setting. SDSU accepts undergraduates and masters students in research, in contrast to some other universities. A quote from this discussion was “there’s no magic line between a MS and PhD student. They both have the potential to achieve great things and have fulfilling experiences”

Dr. Iyer testified that teaching is a very fulfilling experience and can be done in or outside of the classroom. Antenna engineers have to visualize everything that they are doing. We cannot see electromagnetic waves. In Dr. Iyer’s view, people in electromagnetics tend to be exceptional teachers because of the intensity of the necessity of visualization. It’s more important to remember learning how to think and not necessarily about retaining all the tiny details.

After the presentation, attendees enjoyed some refreshments at Starbucks and then took a group photo.

Thank you to Dr. Satish Sharma for organizing a deeply meaningful afternoon for antenna and propagation enthusiasts.

Haifuraiya Flight Hardware Lands in Remote Lab

Information about our terrestrial design progress vs our flight design progress, and why we will have a new development board in Remote Labs West.

Haifuraiya is our microwave-band amateur radio satellite and terrestrial transponder design. Up until now, we’ve used the zcu102 FPGA development board from Xilinx, fitted with an Analog Devices ADRV9002 radio card, to prototype and test the design in the lab and over the air. This has allowed us to make rapid quality progress. Now that we are starting to see end-to-end over-the-air communications results, and now that futureGEO project work is transitioning to CFPs to industry for flight hardware, we need to respond with development equipment that allows flight hardware design, testing, documentation, and acceptable parts lists.

In practice, this means we need a parallel space-oriented development station in addition to the terrestrially-oriented zcu102. The right answer for our design looks to be the vck190. This development board has identical hardware to the space-qualified Versal part that provides what we need to port Haifuraiaya for space.

There are some key differences between the Ultrascale+ part on the zcu102 development board and the Versal part on the vck190.

The Versal chip replaces the classic UltraScale+ DSP48 slices with DSP58 slices. The Versal slices support native floating-point math and wider vector operations. When coding our channelizer and DVB-S2 encoders by hand in RTL, our math blocks “should” synthesize directly into these larger DSP58 structures. Testing will confirm this particular port, but it should be an easy change.

Booting, on the other hand, is radically different. Traditional UltraScale+ parts boot via a master hardware configuration bitstream. The Versal part on the VCK190 boots via a dedicated Platform Management Controller (PMC). The PMC reads a single unified file called a Programmable Device Image (.pdi), which bundles up our FPGA logic, the NoC routing data, and our PetaLinux bootloaders (FSBL/U-Boot) into one package. This is more like the build process for the Pluto than the build process for the zcu102.

Why Use the vck190? Pin and architecture compatibility with the space qualified version of the FPGA part is the big win. The vck190 features the commercial XCVC1902 Versal AI Core, which shares the exact same architecture as the space-qualified XQRVC1902. This allows us to prototype our DSP and RTL logic on the same architecture that will be used in space. This is the first time we’ve stood up specifically space-oriented hardware in Remote Labs.

Development flow is another big reason. We will use the exact same software toolchains (Vivado and Vitis) that we use for terrestrially-oriented designs on the space-grade equivalent.

Space-qualified boards and chips (Class B and Class Y certified) command massive premiums and require specialized handling. The vck190 allows us to iterate and debug your hardware without risking expensive, flight-ready hardware (which can cost tens of thousands of dollars) early in the design cycle. So, we are definitely not too late in the design phase for this equipment upgrade.

But, are we too early? Also no. We have started to see our design work end-to-end in multiple implementations. Now is the time to start porting for space qualified parts, if we want to be ready for both Phase 2 of futureGEO ESA project, and also pitch to US-based satellite companies for ride-shares and hosted payload opportunities.

How do we move to space-grade hardware? First, we’ll continue with extensive simulation with the space-qualified part architecture. Then, we implement on hardware in the lab on the development board, and investigate live signals with integrated logic analyzers and over-the-air metrics. Then, when our design is ready to move from lab testing to custom hardware, we will transition to the space-grade AMD Versal XQR series in a custom board layout.

Instead of the XCVC1902, our flight model will use the XQRVC1902. It is a subtle difference in naming, but there substantial differences between the two parts. The space-grade chip is built with ruggedized, lidless packaging to endure demanding conditions (like much wider thermal variations than commercial or industrial grade, we are talking from -55°C to +125°C) and incorporates built-in circuit techniques to protect against radiation-induced Single Event Upsets (SEUs). There will undoutedly be challenges, setbacks, and learning curves along the way. Our volunteer team is up to the job.

We’ve addressed the FPGA, but what about radio access? Using two identical ADRV9002 cards would simplify the software driver ecosystem. We know how to deal with the 9002. For uplink at 5 GHz, the ADRV9002 can be used directly. However, it cannot handle 10 GHz by itself. For that, we would need something like the ADI XUD1A upconverter.

See the figure for what the lab setup would look like with this configuration. 

We’d use a 7.000 GHz local oscillator at 3.45 GHz IF for the transmit side. The XUD1A gives us 4 independent TX/RX channels. Since Haifuraiya has 64-channel FDMA stream multiplexed into a single TDM carrier, we only need one physical RF stream for the current downlink. This means we will have 3 spare hardware channels on the XUD1A available for multi-antenna array experiments, telemetry, useful beacons, or whatever we can come up with. 

Now, there is some coax connector stuff going on here that we should not ignore. The XUD1A has different connectors than the radio cards. Adapters or additional cables may be necessary.

If you want to be a part of the team, and learn by doing through modern and innovative open source work, please visit https://openresearch.institute/getting-started and sign up. 

Solutions Released for Lunar Descent CTF 

Successfully debuted at BSides San Diego 2026, ORI’s Lunar Descent CTF has been updated with additional documentation and example solutions

One of the many activities that we do at ORI is to participate in and host contests and puzzles. Capture the Flag competitions (CTFs) are a particular type of competition commonly encountered in the cybersecurity and hacking communities. CTFs pose a set of challenges for participants to solve, often drawn from a particular theme or subject. CTFs can be tackled by individuals, but the interdisciplinary and complex nature of many CTFs require a team working together in order to score enough points to be at the top of the leader board.

The Lunar Descent CTF debuted at BSides San Diego, held at San Diego State Univsity on 4 April 2026. This is an ORI original, and all documents can be found on GitHub at https://github.com/OpenResearchInstitute/lunar-descent-ctf. The CTF is based on a real signal processing problem in a radar altimeter.

ISRO’s KaRA radar altimeter guided Chandrayaan-3 to a soft lunar landing on 23 August 2023. The Radar Altimeter Processor (RAP) computes altitude and velocity from FMCW chirp signals, running on a single Xilinx Virtex-5 FPGA. This CTF uses a Python model of that system, faithful to the published paper, where the altimeter feeds a landing autopilot. The altimeter works perfectly. However, once the system was operational, the autopilot keeps crashing in last-minute testing. Why? The answer is the solution to the CTF. 

The Lunar Descent CTF is self-scoring and self-paced, which reduced the workload of the booth volunteers. A copy of the IEEE Aerospace and Electronics System Society Magazine article that inspired the CTF was available for people to read. ORI-themed USB drives with a copy of the CTF repository contents were given away to anyone that wanted one to take home with them. The CTF attracted a lof of attention at the ORI-supported RF Village at BSides San Diego, and reviews from participants were very good. While it was anticipated that some participants would be able to solve the CTF in two hours or so, it took the first place winner most of the day, as they wanted to see all the other villages at BSides, and also attend talks. The self-paced “take home” format greatly reduced the pressure on the participants to commit to a contest over seeing the rest of the show. We received positive feedback about this decision, and will use the self-scoring and self-paged methodology in future CTFs. This approach was inspired by the self-scoring BLE CTF, which can be found at https://github.com/hackgnar/ble_ctf

If you would l like to try the CTF, then clone the lunar-descent-ctf repository, start with the top-level README.md, and avoid looking in the spoilers/ directory. The spoilers/ directory has a README file for staff running the event, detailed directions on how to score challenge #1, and also has two example solutions for challenge #2 and challenge #3. Since the solutions are tucked away into a separate directory, one can clone the repository and attempt the CTF without accidentally seeing any of the solutions or hints. However, if you get stuck, or want to compare your solution to the example solutions, all you need to do is drop down into the spoilers/ directory and read through the documentation and solutions.

If you want to use this CTF at your own event, please feel free to clone it and adapt it for your setting and audience.

ORI futureGEO HAMRADIO 2026 Workshop Report

ORI participated in the futureGEO Community Workshop at HAMRADIO 2026. Held annually in Friedrichshafen, Germany, HAMRADIO is the largest amateur radio event in Europe, attracting 15,000 people from 50 countries. The workshop was 4:00 pm – 5:30 pm on 27 June 2026 and filled the capacity 40 room.

The description of the workshop was “ESA, in collaboration with AMSAT-DL and the international amateur satellite community, intends to assess the feasibility of designing, developing, and operating an advanced satellite communications payload suitable for supporting in-orbit experimentation by the amateur satellite community in GEO-orbit. During this workshop we want to present 2 to 3 different consolidated amateur satellite mission concepts from the study. Further we want to collect feedback from the community for a final proposal.”

The futureGEO workshop at HAMRADIO 2026. At the desk in front, Peter Gülzow, president of AMSAT-DL, presents about the history and context of QO-100. Frank Zeppenfeldt was the second speaker, and defined the ESA's role with futureGEO, how Phase 1 would conclude, and what Phase 2 would entail. Michelle Thompson (far left) was the third and final speaker, and presented the working prototype from ORI for futureGEO submission.

Peter Gülzow, president of AMSAT-DL, opened the workshop with a summary of QO-100 history and context. He shared that the operator (Es’Hail) expects another 9 years of life for the satellite. This means that we are a bit less than half-way through the lifetime of QO-100 transponder.

Peter introduced three potential categories of amateur radio satellite spacecraft.

  • Enhanced QO-100+ Bent Pipe
  • Digital Innovation Lab
  • High Frequency Pathfinder

These appear to be very high-level “consolidated mission concepts” from the workshop description.

The next speaker was Frank Zeppenfeldt, PD0AP (M2M, IoT, Smallsats and Spectrum at European Space Agency). He explained that planning for what comes after QO-100 is the primary motivation of ESA’s futureGEO project. Frank said that a futureGEO payload would almost surely be built by industry, and that this workshop was intended to close out Phase 1 of the futureGEO project, and that a report would be written and published about Phase 1 in August 2026.

What is futureGEO?

The FutureGEO project is an ESA (European Space Agency) initiative to develop a future amateur radio payload for a geostationary satellite. The aim is to identify potential partners who would like to actively participate in the definition and development of a new amateur radio payload for a future geostationary satellite. 

ESA proposed the idea of a geosynchronous satellite back in December of 2023. Frank secured €250,000 in funding to investigate the possibility of an amateur satellite or payload in geostationary orbit. The announcement was made in a presentation at the AMSAT-UK Colloquium.

ORI’s Presentation

Michelle Thompson was the third and final presenter at the workshop, speaking on behalf of ORI’s futureGEO proposal team. ORI is a signatory to the letter of interest (LOI) from AMSAT-DL, participated in the 2025 futureGEO Workshop at AMSAT-DL Symposium, and has submitted a one-page proposal as well as a white paper about ORI’s proposed design. Both of these documents can be found in the futureGEO GitLab as well as at the above links.

Michelle described the working hardware, firmware, and software implementations of Haifuraiya, or “High Flyer”. Haifuraiya is a functional prototype digital regenerative multiplexing amateur radio satellite system, with superior voice quality and integrated voice, text, and data. There are three implementations of the Opulent Voice ground station, and two implementations of the satellite segment. Processing occurs in the satellite. This is not a double-hop system. Uplink is frequency division multiple access Opulent Voice and downlink is DVB-S2 time-division multiplex. The design is carefully engineered and tested, completely open source, and fully documented. This poster summarizes the status of ORI’s proposal for futureGEO as of June 2026.

Slide from the talk presenting the design:


Download original PDF of the presentation poster below:

The poster was displayed at the AMSAT-DL booth for the three days of the show. There was consistent, strong, positive feedback for the design. Questions from the show participants were intelligent and meaningful, ranging from UX/UI theory and operations to the specific mathematics of the demodulator.

AMSAT-DL kindly and generously supported ORI with space and time to communicate a real-life working implementation of the futureGEO concept. ORI takes the futureGEO project seriously, and will complete both a terrestrial repeater version as well as a space-qualified communications board prototype of Haifuraiya.

ORI will participate in Phase 2 of futureGEO, and looks forward to the next steps of the project.