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- All Graduate Theses and Dissertations, Spring 1920 to Summer 2023 (9)
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Articles 1 - 30 of 34
Full-Text Articles in Engineering
The Active Cryocubesat Technology: Active Thermal Control For Small Satellites, Lucas S. Anderson
The Active Cryocubesat Technology: Active Thermal Control For Small Satellites, Lucas S. Anderson
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Modern CubeSats and Small Satellites have advanced in capability to tackle science and technology missions that would usually be reserved for more traditional, large satellites. However, this rapid growth in capability is only possible through the fast-to-production, low-cost, and advanced technology approach used by modern small satellite engineers. Advanced technologies in power generation, energy storage, and high-power density electronics have naturally led to a thermal bottleneck, where CubeSats and Small Satellites can generate more power than they can easily reject. The Active CryoCubeSat (ACCS) is an advanced active thermal control technology (ATC) for Small Satellites and CubeSats, which hopes to …
Implementation Of The Downlink Communication System Of The Lmu Cubesat, Mohammed Alrabeeah
Implementation Of The Downlink Communication System Of The Lmu Cubesat, Mohammed Alrabeeah
LMU/LLS Theses and Dissertations
In this thesis, we present the design and implementation of a CubeSat receiver system using the Universal Software Radio Peripheral (USRP) and GNU Radio. The goal of this project is to develop a low-cost and flexible ground station capable of receiving telemetry and payload data from CubeSats in real time. The CubeSat receiver operates in the UHF frequency range with a center frequency of 435 MHz and uses a software-defined radio (SDR) approach to provide wideband signal processing and demodulation capabilities. The satellite transceiver transmits an Ax.25 Transciever packet every 1 second using the Pumpkin CubeSat kit programmed in MPLab. …
High-Isolation Antenna Technique For Cubesat-Borne, Continuous-Waveform Radar, Logan E. Voigt
High-Isolation Antenna Technique For Cubesat-Borne, Continuous-Waveform Radar, Logan E. Voigt
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Radar is important in target tracking, imaging, and weather prediction applications. As technology is increasingly miniaturized, there is a push for smaller radar. Research and exploration in outer space also benefit from small, low-power technologies. The NASA Jet Propulsion Laboratory’s RainCube was the first successful CubeSat-borne radar. A CubeSat is a type of small satellite that conforms to specific size and weight standards. Radar technology benefits from additional research on how to further miniaturize radar payloads.
Integrating the transmit and receive antennas on the solar panels removes the need for antenna-deployment mechanisms, preserving space on the CubeSat. This thesis also …
Design, Implementation, And Test Of Spacecraft Antennae And A Ground Station For Mesat1, Travis Russell
Design, Implementation, And Test Of Spacecraft Antennae And A Ground Station For Mesat1, Travis Russell
Electronic Theses and Dissertations
MESAT1 is a CubeSat that was proposed by the University of Maine in response to NASA's CubeSat Launch Initiative, and in early 2020 was selected by NASA to be launched into a Low Earth Orbit (LEO) in June of 2022. The satellite will carry four low-cost complementary metal–oxide–semiconductor (CMOS) cameras which serve as sensing instruments for three science missions proposed by K-12 schools in Maine. The cameras will periodically take pictures of Earth to analyze water turbidity, identify urban heat islands, and predict harmful algal blooms. The multi-spectral image data is packed into frames and downlinked as Binary Phase-Shift Keying …
Failure Mode, Effects And Criticality Analysis Of A Very Low Earth Orbit Cubesat Mission, Robb Christopher Borowicz
Failure Mode, Effects And Criticality Analysis Of A Very Low Earth Orbit Cubesat Mission, Robb Christopher Borowicz
Mechanical & Aerospace Engineering Theses & Dissertations
When space programs launch vehicles into orbit, multiple failures could arise throughout the mission and corrective actions are often not an option. Applying reliability engineering approaches during the design phase focuses on analyzing risk by anticipating potential failures and mitigating uncertainties in the design. Old Dominion University, in partnership with the U.S. Coast Guard Academy, and the U.S. Air Force Institute of Technology designed and developed a 3U CubeSat mission to validate on-orbit, three space technology payloads. Mission SeaLion will fly as a secondary payload on stage two of Northrop Grumman’s Antares rocket and will be deployed in a very …
Utilization Of Characteristic Modal Analysis For Antenna Design Needed For An Afit Satellite, Scott C. Podlogar
Utilization Of Characteristic Modal Analysis For Antenna Design Needed For An Afit Satellite, Scott C. Podlogar
Theses and Dissertations
Antenna design is a pervasive, growing field for electrical engineers. As the number of new materials and techniques increase so too does the demand and requirements pushing forth new innovative ideas. Among these ideas is a leading edge analytic technique called Characteristic Modal Analysis (CMA) originally credited to Garbacz and Turpin. CMA works to break down the current distribution along a structure in a way that can offer great insights into how that structure operates as an antenna. This technique has great merits in post design analytics but it is rarely seen to be integrated into the design process. This …
Design Of Miniaturized Sweeping Langmuir Probe And Electric Field Probe For The Sport Mission, Nathan P. Tipton
Design Of Miniaturized Sweeping Langmuir Probe And Electric Field Probe For The Sport Mission, Nathan P. Tipton
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
The Scintillation Prediction Observation Research Task (SPORT) is a joint United States of America and Brazil 6U CubeSat mission. The US is providing the science instruments and the spacecraft launch. Brazil is providing the spacecraft bus, integration, and operations. Utah State University will provide four instruments for the mission as part of the US contribution in a suite called the Space Weather Probes (SWP). These instruments are the Sweeping Langmuir Probe (SLP), the Electric Field Probe (EFP), and the Sweeping Impedance Probe (SIP). Higher frequency components of the SLP and EFP will be observed through a Wave Spectrometer (WS). These …
System Level Characterization Of The Gridded Retarding Ion Drift Sensor (Grids) For The Petitsat Mission, Benjamin B. Oborn
System Level Characterization Of The Gridded Retarding Ion Drift Sensor (Grids) For The Petitsat Mission, Benjamin B. Oborn
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Weather prediction, wherever people live, serves as a beneficial part of everyday life. Weather in the upper portions of Earth’s atmosphere also impacts life on Earth but it is not able to be predicted as well as its terrestrial counterpart. PetitSat is a cube satellite (CubeSat) mission proposed to help remedy this issue. It will collect measurements of charged particles in the upper atmosphere called a plasma. The measurements taken by PetitSat will facilitate better prediction of upper-atmospheric weather. Prediction of when and where weather phenomenon will occur will allow avoidance of negative consequences that can result. Once such negative …
Applying Internet Of Things Principles To Spacecraft, Brian K. Dixon
Applying Internet Of Things Principles To Spacecraft, Brian K. Dixon
Theses and Dissertations
This thesis proposes the adaptation of the IEEE 1451 Transducer Electronic Data Sheet (TEDS) for usage in spacecraft subsystems. In the 1990s, TEDS initially were developed as a standardized method to provide metadata required for the operation of a transducer by a microcontroller or data acquisition device. The metadata provides information that identifies and documents key characteristics of the transducer, thereby facilitating plug-and-play interoperability within a system and across networks. An overarching goal of this thesis is to make a case for adapting and extending the TEDS concept as a means for self-describing critical physical components of a CubeSat nanosatellite. …
Design, Implementation, And Analysis Of Electrical System Architecture For Cubesat To Ground Communications, Anthony G. Cappiello
Design, Implementation, And Analysis Of Electrical System Architecture For Cubesat To Ground Communications, Anthony G. Cappiello
Electrical & Computer Engineering Theses & Dissertations
CubeSats facilitate a low barrier to entry in University and Industrial space research. With the rapid, low-cost development of CubeSats, the need for a reliable and ro- bust communications subsystem becomes evident to ensure mission accomplishment. With the advent of Software Defined Radio, Old Dominion University is compelled to upgrade the rigid Legacy Hardware systems in place with inexpensive and flexible Software Defined Radio Solutions. Currently, Old Dominion University is on the cusp of conducting its first space science mission as a member organization of the Virginia Space Grant Consortium Cubesat Constellation and is manifest for launch on April 17, …
Cloudsat: Iot Approach To Small Satellite Ground Infrastructure, Brian Zufelt
Cloudsat: Iot Approach To Small Satellite Ground Infrastructure, Brian Zufelt
Electrical and Computer Engineering ETDs
Over the last decade, the cost of space access has dramatically decreased with the creation of the CubeSat standard. The CubeSat standard defines the structural requirements for an on-orbit deployer and satellite to be placed into orbit. The average cost of creating a space mission with the CubeSat standard can range from $200 thousand to over $3 million. This lower cost has allowed many Universities, and small businesses to create their own space programs. However, a significant portion of the investment for any new space asset is the development of the ground system to communicate with the satellite. These costs …
Software Defined Radio For Cubesat Communication, Sarah Watkins
Software Defined Radio For Cubesat Communication, Sarah Watkins
Undergraduate Honors Capstone Projects
Cube satellites, more commonly referred to as CubeSats, are small satellites that have become increasingly popular for academic, amateur, commercial, and scientific applications over the past five to ten years. These satellites provide a fairly inexpensive and compact platform for deploying many different types of equipment. While CubeSats do not allow for housing large, complex instruments, some organizations have begun to explore the possibility of deploying networks, or clusters, of CubeSats. Satellites in these clusters could theoretically be tied together via radio frequency communications to accomplish more than a single CubeSat could alone.
This report summarizes the preliminary design and …
Cubesat Data Transmission And Storage Throughput Optimization Through The Use Of A Zynq Soc Based Cubesat Science Instrument Interface Electronics Board, Caleb Mosby Munsill
Cubesat Data Transmission And Storage Throughput Optimization Through The Use Of A Zynq Soc Based Cubesat Science Instrument Interface Electronics Board, Caleb Mosby Munsill
Master's Theses
The CubeSat standard sprang from the desire to create a satellite standard that would open the doors for universities and other lower budget research institutions by making it more feasible to get their work into space. Since then, many other institutions and industries have been adopting variations on the standard for their own use. As more people are seeking out to use the CubeSat standard as their main bus, the standards and practices of the community have grown and expanded and with this growth, new challenges have been created. One such challenge is the bandwidth limitation in the RF-downlink. When …
Transparent Solar Panel Antenna Array, Taha Shahvirdi Dizaj Yekan
Transparent Solar Panel Antenna Array, Taha Shahvirdi Dizaj Yekan
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
A CubeSat is a very small satellite that has been achieving growing interests in space exploration. The base unit of CubeSats 1U, which is a cube with 10 cm on each side. In applications, CubeSats can be deployed as just 1U, or multiple unites can be stacked together to form a larger CubeSat for extended functionality. Due to their small sizes, it is challenging to fit antennas onto CubeSats because the antenna always fights for surface real estate with solar cells. The challenge is further aggravated when an antenna is required to have high gain such as more than 20 …
Plasma Velocity Vector Instrument For Small Satellites (Pvviss), William Smith Hatch
Plasma Velocity Vector Instrument For Small Satellites (Pvviss), William Smith Hatch
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Low-earth orbit (LEO) contains plasma which can impact satellite charging and radio frequency (RF) communications. Quantifying both the composition and movement of ions in LEO can improve efficiency of the forecasting models that predict the impact plasma will have on satellite communications and accuracy of global positioning satellite measurements.
Two instruments known as the Retarding Potential Analyzer (RPA) and the Ion Drift Meter (IDM) have been used in tandem to measure ionospheric properties including ion temperature, velocity, and density. These instruments are costly and occupy large areas on a spacecraft. In recent years, space mission budgets have diminished. This change …
Design Of Miniaturized Time-Of-Flight Reflectron Mass Spectrometer For Upper Atmosphere Density Measurements, Michelle Lynn Pyle
Design Of Miniaturized Time-Of-Flight Reflectron Mass Spectrometer For Upper Atmosphere Density Measurements, Michelle Lynn Pyle
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Upper atmosphere and solar events can have strong impacts on the communication, power, and navigation systems we use every day. Modeling atmospheric dynamics, or the changes and reactions of different regions of the atmosphere, can help improve understanding and predictions of the effects of solar events. A suite of measurements of the upper atmosphere, including wind, temperature, and composition measurements, is used to build atmospheric models. Current atmospheric models are very sophisticated but need additional data to fully model atmospheric dynamics. In the past, measurements used to determine atmospheric composition have been performed using mass spectrometer instruments on full-size satellites. …
Ism S-Band Cubesat Radio Designed For The Polysat System Board, Craig Lee Francis
Ism S-Band Cubesat Radio Designed For The Polysat System Board, Craig Lee Francis
Master's Theses
Cal Poly’s PolySat CubeSat satellites have begun to conduct more complex and scientifically significant experiments. The large data products generated by these missions demonstrate the necessity for higher data rate communication than currently provided by the PolySat UHF radio. This thesis leverages the proliferation of consumer wireless monolithic transceivers to develop a 250kbps to 2000kbps, 2W CubeSat radio operating within the 2.45GHz Industrial, Scientific, and Medical (ISM) radio band.
Estimating a link budget for a realistic CubeSat leads to the conclusion that this system will require a large deployable CubeSat antenna, large earth station satellite dish, and a fine-pointing attitude …
Cubesat Electronic Power System, Benjamin Lynch, Callie Wallace
Cubesat Electronic Power System, Benjamin Lynch, Callie Wallace
Electrical and Computer Engineering Senior Theses
Cube Satellites are small satellites used by NASA and other non-governmental space companies as a cost-effective means to get a payload into space to perform research and develop new technologies. The Robotic Systems Lab at Santa Clara University has designed and launched several Cube Satellites over the last ten years. We will be continuing the design of a 3U CubeSat began by a senior design team last year. The goal of this project is to design and build an electronic power system (EPS) for the CubeSat. The EPS must be able to power all system components, including the communication board, …
Dual High-Voltage Power Supply For Use On Board A Cubesat, Nicholas Weiser
Dual High-Voltage Power Supply For Use On Board A Cubesat, Nicholas Weiser
Master's Theses
Since their conception in 1999, CubeSats have come and gone a long way. The first few that went into space were more of a “proof of concept,” and were more focused on sending simple data and photographs back to Earth. Since then, vast improvements have been made by over 40 universities and private firms, and now CubeSats are beginning to look towards interplanetary travel. These small satellites could provide a cost effective means of exploring the galaxy, using off the shelf components and piggy-backing on other launch vehicles with more expensive payloads. However, CubeSats are traditionally launched into Low Earth …
Proposed Middleware Solution For Resource-Constrained Distributed Embedded Networks, Jason T. Rexroat
Proposed Middleware Solution For Resource-Constrained Distributed Embedded Networks, Jason T. Rexroat
Theses and Dissertations--Electrical and Computer Engineering
The explosion in processing power of embedded systems has enabled distributed embedded networks to perform more complicated tasks. Middleware are sets of encapsulations of common and network/operating system-specific functionality into generic, reusable frameworks to manage such distributed networks. This thesis will survey and categorize popular middleware implementations into three adapted layers: host-infrastructure, distribution, and common services. This thesis will then apply a quantitative approach to grading and proposing a single middleware solution from all layers for two target platforms: CubeSats and autonomous unmanned aerial vehicles (UAVs). CubeSats are 10x10x10cm nanosatellites that are popular university-level space missions, and impose power and …
A Compact, Reconfigurable Uhf Communication System Design For Use With Polysat's Embedded Linux Platform, Austin Williams
A Compact, Reconfigurable Uhf Communication System Design For Use With Polysat's Embedded Linux Platform, Austin Williams
Master's Theses
The beginning of this thesis provides an overview of the heritage UHF Communication System design flown on CP2, CP3, CP4, CP5, and CP6, summarizing previous analysis of its performance, and providing the justification for a complete system re-design. High level requirements for the new UHF System are defined, and a trade study is performed on state-of-the-art single chip transceivers, low noise amplifiers, and transmit power amplifiers. These components are then designed into a functional communication system, with key components analyzed for proper impedance matching and performance characterization compared to expected datasheet values. Next, the system as a whole is characterized …
Cubesat Launch Sequencer, Billy Beecher
Cubesat Launch Sequencer, Billy Beecher
Electrical Engineering
I am working with the Naval Postgraduate School to develop a low cost CubeSat launch sequencer for NPSCuL that is designed to operate in low Earth orbit. The system will be capable of providing programmable delays with a minimum delay of one second to a maximum delay of five minutes. Delays must be accurate to within ± 10% or within one second, whichever is less. After the delay, the system will provide the necessary launch signal. To ensure protection from radiation, the system will feature triple redundancy and voting logic stages to ensure that the proper signal is propagated.
Optical Sensors For Mapping Temperature And Winds In The Thermosphere From A Cubesat Platform, Stephanie Whalen Sullivan
Optical Sensors For Mapping Temperature And Winds In The Thermosphere From A Cubesat Platform, Stephanie Whalen Sullivan
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
In the same way that mariners desire to know the weather their ships are about to encounter, satellite owners would like to know the conditions along their satellites' orbits. Accurate forecasts would allow operators to secure sensitive components prior to passing through a storm to reduce the risk of damage. Large solar arrays, which can act like sails, can be re-oriented to prevent the satellite from being moved out of its desired orbit. While terrestrial weather forecasters have thousands of sensors with continuous data streams available to generate weather models, very few sensors exist for space weather. Cost of sensing …
Providing A Persistent Space Plug-And-Play Avionics Network On The International Space Station, Zachary A. Jacobs
Providing A Persistent Space Plug-And-Play Avionics Network On The International Space Station, Zachary A. Jacobs
Theses and Dissertations--Electrical and Computer Engineering
The CubeLab is a new payload standard that greatly improves access to the International Space Station (ISS) for small, rapid turn-around microgravity experiments. CubeLabs are small (less than 16”x8”x4” and under 10kg) modular payloads that interface with the NanoRacks Platform aboard the ISS. CubeLabs receive power from the station and transfer data using the standard terrestrial plug-and-play Universal Serial Bus (USB). The Space Plug-and-play Avionics (SPA) architecture is a modular technology for spacecraft that provides an infrastructure for modular satellite components to reduce the time to orbit and development costs for satellites. This paper describes the development of a bus …
An Attitude Determination System With Mems Gyroscope Drift Compensation For Small Satellites, Maxwell Bezold
An Attitude Determination System With Mems Gyroscope Drift Compensation For Small Satellites, Maxwell Bezold
Theses and Dissertations--Electrical and Computer Engineering
This thesis presents the design of an attitude determination system for small satellites that automatically corrects for attitude drift. Existing attitude determination systems suffer from attitude drift due to the integration of noisy rate gyro sensors used to measure the change in attitude. This attitude drift leads to a gradual loss in attitude knowledge, as error between the estimated attitude and the actual attitude increases.
In this thesis a Kalman filter is used to complete sensor fusion which combines sensor observations with a projected attitude based on the dynamics of the satellite. The system proposed in this thesis also utilizes …
Radio Link Analysis And Characterization Of Past And Future Cal Poly Cubesats, Brian Gilbert Tubb
Radio Link Analysis And Characterization Of Past And Future Cal Poly Cubesats, Brian Gilbert Tubb
Electrical Engineering
Cal Poly's satellites design team, PolySat, has three satellites in Low Earth Orbit (LEO) and four more planned to launch within the next two years. Radio communication of past and current orbiting satellites has been an exercise in frustration, prompting significant research into the satellite-side of the radio link by several other Senior Projects and Thesis papers. However, minimal effort has been spent on evaluating why these problems were discovered only once the satellites reached orbit. This paper details the downfalls of relying heavily on link budgets and improper long range test setups, then experimentally determines the sensitivity of PolySat's …
Day/Night Band Imager For A Cubesat, Eric Stanton
Day/Night Band Imager For A Cubesat, Eric Stanton
Electrical Engineering
Day/Night Band (DNB) earth sensing and meteorological systems like the Defense Meteorological Satellite Program (DMSP) Operational Linescan System (OLS) provide visible wavelength imagery 24 hours a day that is used primarily for cloud imaging in support of weather forecasting. This paper describes a compact push-broom imager that meets low light imaging requirements for DMSP OLS and the NOAA/NASA Joint Polar Satellite System (JPSS) as documented in the Integrated Operational Requirements Document [1] (IORD) including the imager design, system level concepts of operation for data collection, radiometric and spatial calibration, and data transmission to Earth. This small, lightweight imager complies with …
Reliable Software Updates For On-Orbit Cubesat Satellites, Sean Fitzsimmons
Reliable Software Updates For On-Orbit Cubesat Satellites, Sean Fitzsimmons
Master's Theses
CubeSat satellites have redefined the standard solution for conducting missions in space due to their unique form factor and cost. The harsh environment of space necessitates examining features that improve satellite robustness and ultimately extend lifetime, which is typical and vital for mission success. The CubeSat development team at Cal Poly, PolySat, has recently redefined its standard avionics platform to support more complex mission capabilities with this robustness in mind. A significant addition was the integration of the Linux operating system, which provides the flexibility to develop much more elaborate protection mechanisms within software, such as support for remote on-orbit …
Three-Dimensional Structural Electronic Integration For Small Satellite Fabrication, Cassie Gutierrez
Three-Dimensional Structural Electronic Integration For Small Satellite Fabrication, Cassie Gutierrez
Open Access Theses & Dissertations
The ability to realize truly three-dimensional electronic circuits is complicated if not impossible using traditional fabrication techniques. Such techniques are limited to the use of two dimensional printed circuit boards (PCBs), and require various dissonant processes which exhaust time, volume and cost. Due to the nature of Additive Manufacturing (AM) such problems are diminished and in some ways completely overcome. Additive Manufacturing allows for a higher range of design freedom along conformal surfaces, as well as unit level customization; it is the threshold for embedded electronics, allowing for three-dimensional circuitry in ways traditional fabrication is unfeasible. In such ways, additive …
A Two-Dimensional Numerical Simulation Of Plasma Wake Structure Around A Cubesat, Rajendra Mitharwal
A Two-Dimensional Numerical Simulation Of Plasma Wake Structure Around A Cubesat, Rajendra Mitharwal
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
A numerical model was developed to understand the time evolution of a wake structure around a CubeSat moving in a plasma with transonic speed. A cubeSat operates in the F2 layer of ionosphere with an altitude of 300 − 600 Km. The average plasma density varies between 10−6cm−3 − 10−9cm−3 and the temperature of ions and electrons is found between 0.1−0.2 eV. The study of a wake structure can provide insights for its effects on the measurements obtained from space instruments. The CubeSat is modeled to have a metal surface, which is a realistic …