Radio Aurora Explorer: A Mission Overview

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140647/1/1.a32436.pd

On-Orbit Calibration of Photodiodes for Attitude Determination

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140645/1/1.g000175.pd

Large-Scale Multidisciplinary Optimization of a Small Satellite’s Design and Operation

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140669/1/1.a32751.pd

Expanding the Capability of Satellite Operations using a Global Federated Ground Station Network

Small-scale spaceflight programs such as those found at universities and start-up companies may operate satellites from a single ground station. This station’s location may not be optimal for radio communications, and a single station limits the contact time available to conduct operations. The idea of a global federated ground station network (FGN) has been theorized in the past, and with today’s wide-spread internet connectivity it is now possible for such a network to exist. One example of an FGN that is functioning today is an open-source project called SatNOGS. The Michigan eXploration Laboratory (MXL) at the University of Michigan has applied the benefits of this network to enhance operations of their Tandem Beacon Experiment (TBEx) CubeSat mission by gathering 2.2x the beacons gathered by their home station alone. 93% of those additional beacons were collected by six SatNOGS stations. Augmenting MXL’s home station with these six stations increases access time to the TBEx satellites by a factor of 5 to15. This increased temporal coverage also enabled MXL operators to identify their spacecraft after deployment and correct an error causing the TBEx radios to function intermittently, saving the mission in its earliest days

Radar and rocket comparison of UHF radar scattering from auroral electrojet irregularities: Implications for a nanosatellite radar

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/95174/1/jgra19910.pd

A Fractionated Space Weather Base at L_5 using CubeSats and Solar Sails

The Sun–Earth L_5 Lagrange point is an ideal location for an operational space weather forecasting mission to provide early warning of Earth-directed solar storms (coronal mass ejections, shocks and associated solar energetic particles). Such storms can cause damage to power grids, spacecraft, communications systems and astronauts, but these effects can be mitigated if early warning is received. Space weather missions at L5 have been proposed using conventional spacecraft and chemical propulsion at costs of hundreds of millions of dollars. Here we describe a mission concept that could accomplish many of the goals at a much lower cost by dividing the payload among a cluster of interplanetary CubeSats that reach orbits around L5 using solar sails

Design and Implementation of the GPS Subsystem for the Radio Aurora Explorer

Abstract This paper presents the design and implementation of the Global Positioning System (GPS) subsystem for the Radio Aurora eXplorer (RAX) CubeSat. The GPS subsystem provides accurate temporal and spatial information necessary to satisfy the science objectives of the RAX mission. There are many challenges in the successful design and implementation of a GPS subsystem for a CubeSat-based mission, including power, size, mass, and financial constraints. This paper presents an approach for selecting and testing the individual and integrated GPS subsystem components, including the receiver, antenna, low noise amplifier, and supporting circuitry. The procedures to numerically evaluate the GPS link budget and test the subsystem components at various stages of system integration are described. Performance results for simulated tests in the terrestrial and orbital environments are provided, including start-up times, carrier-to-noise ratios, and orbital position accuracy. Preliminary on-orbit GPS results from the RAX-1 and RAX-2 spacecraft are presented to validate the design process and pre-flight simulations. Overall, this paper provides a systematic approach to aid future satellite designers in implementing and verifying GPS subsystems for resourceconstrained small satellites