Award Abstract # 1936567
Collaborative Research: CubeSat Ideas Lab: VIrtual Super-resolution Optics with Reconfigurable Swarms (VISORS)

NSF Org: AGS
Division of Atmospheric and Geospace Sciences
Recipient: NEW MEXICO STATE UNIVERSITY
Initial Amendment Date: August 16, 2019
Latest Amendment Date: July 29, 2022
Award Number: 1936567
Award Instrument: Continuing Grant
Program Manager: Mangala Sharma
msharma@nsf.gov
 (703)292-4773
AGS
 Division of Atmospheric and Geospace Sciences
GEO
 Directorate for Geosciences
Start Date: October 1, 2019
End Date: September 30, 2023 (Estimated)
Total Intended Award Amount: $70,014.00
Total Awarded Amount to Date: $70,014.00
Funds Obligated to Date: FY 2019 = $27,500.00
FY 2020 = $28,324.00

FY 2021 = $3,466.00

FY 2022 = $10,724.00
History of Investigator:
  • Hyeongjun Park (Principal Investigator)
    hjpark@nmsu.edu
Recipient Sponsored Research Office: New Mexico State University
1050 STEWART ST.
LAS CRUCES
NM  US  88003
(575)646-1590
Sponsor Congressional District: 02
Primary Place of Performance: New Mexico State University
Las Cruces
NM  US  88003-8002
Primary Place of Performance
Congressional District:
02
Unique Entity Identifier (UEI): J3M5GZAT8N85
Parent UEI:
NSF Program(s): Space Weather Research
Primary Program Source: 01001920DB NSF RESEARCH & RELATED ACTIVIT
01002021DB NSF RESEARCH & RELATED ACTIVIT

01002122DB NSF RESEARCH & RELATED ACTIVIT

01002223DB NSF RESEARCH & RELATED ACTIVIT
Program Reference Code(s): 8092, 9150
Program Element Code(s): 808900
Award Agency Code: 4900
Fund Agency Code: 4900
Assistance Listing Number(s): 47.050

ABSTRACT

CubeSats are miniaturized, low-weight, low-cost satellites. Due to these properties, constellations of 10s-100s of CubeSats with specialized instruments for studying the space environment provide a new exciting opportunity to understand and predict space weather. The Virtual Super-resolution Optics with Reconfigurable Swarms (VISORS) mission supports the advancement of using constellations of CubeSats for space weather through designing, building, and operating three satellites that together form an ultraviolet telescope for observing the Sun. VISORS has a transformative technological approach; it will be the first distributed telescope using several breakthrough technologies, including: novel photon sieve optics, precision formation flying, and 5G-inspired high data rate communications between the spacecraft. The transformative optics utilized by the mission will allow high spatial and temporal observations of nanoflares that are potentially an important source of heating of the solar corona. The VISORS mission supports STEM education and public outreach. Graduate and undergraduate students will actively participate in all mission stages. The project will also develop an open-source software toolkit to support the design and optimization of CubeSat that can be utilized in classrooms. Further, a hands-on demonstration of the virtual telescope will be developed for a science museum exhibit. This project resulted from the Ideas Lab: Cross-cutting Initiative in CubeSat Innovations, an interdisciplinary program supported by Geosciences, Engineering, and Computer and Information Science and Engineering Directorates.

VISORS will provide a transformational leap in addressing the origins of the processes heating the solar corona by revealing filamentary coronal structures as narrow as 160 milliarcseconds and use the spatial and temporal characteristics of those structures to constrain physical models of nanoflares much more powerfully than the indirect methods used to date. In addition to addressing one of the most fundamental open questions in geospace science, VISORS will validate several breakthrough technologies. The technological innovations range from the demonstration of the first distributed ultraviolet telescope with unprecedented angular resolution, novel photon sieve optics, and CubeSat precision formation flying, to the demonstration of sub-kilometer proximity operations on CubeSat swarms, including low-interference propulsive maneuvers; navigation, control, and autonomy; and 5G-inspired high data-rate inter-CubeSat swarm communication and networking.

This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

PROJECT OUTCOMES REPORT

Disclaimer

This Project Outcomes Report for the General Public is displayed verbatim as submitted by the Principal Investigator (PI) for this award. Any opinions, findings, and conclusions or recommendations expressed in this Report are those of the PI and do not necessarily reflect the views of the National Science Foundation; NSF has not approved or endorsed its content.

The VIrtual Super-resolution Optics with Reconfigurable Swarms (VISORS) mission’s major goal is to understand the origin and dynamic evolution of solar coronal plasma by demonstrating a novel and scalable imaging technology with a virtual super-resolution telescope using diffractive optics, inter-satellite crosslinks, and CubeSat precision formation flying. The VISORS mission is designed to provide a high-success, low-risk mission that is inherently safe to operate using advanced formation flying methods for multiple CubeSats, 3D-printed propulsion systems, and a high throughput inter-satellite crosslink. 

In this project, the New Mexico State University (NMSU) team performed basic and applied research to achieve the major goal and critical technical requirements of the collaborative research, that is precision formation flying and attitude alignment for multiple CubeSats. To achieve the institutional goal, we simulated, evaluated, and verified the capability of the attitude determination and control system (ADCS) provided by Blue Canyon Technologies in the science observation mode considering the environmental disturbances and system uncertainties. Also, we verified various scenarios of the ADCS for the concept of operations (ConOps), as well as analyzed the attitude profile and keep-out zone constraints of the ConOps including the observation mode, science mode, and the transition modes. To determine the maximum delta-V that can be executed without saturating reaction wheels, we developed an algorithm to convert from the propulsion frame orientation to the orbit’s local frame and analyzed reaction wheel desaturation and momentum budget. Finally, we developed an algorithm to send realistic control commands from the ADCS to the propulsion system considering the limited thrust force. For simulating the developed algorithms, we developed a MATLAB/Simulink-based CubeSat maneuvering simulator.

This project provided opportunities for individual study courses and master thesis topics for graduate students and training undergraduate students including two female engineering students: one is a graduate student who worked her master's program on CubeSat attitude determination and control and the other is an undergraduate student who was trained with the hands-on experiences for simulations of ADCS. The developed simulation models and methods were introduced to the student members of the small satellite development team at NMSU, which is a Minority Serving Institute. The developed MATLAB/Simulink simulator of slew maneuvering of CubeSats was utilized to teach attitude control systems for undergraduate and graduate students. The results and lessons learned from this research were shared with the NMSU NanoSat Lab team members. 

Distributed spacecraft systems have revolutionized a new class of missions for navigation, communications, remote sensing, and scientific research for civilian and military purposes. In particular, virtual telescopes composed of CubeSats are being used for higher-resolution imaging. We developed a simulation environment to verify the capability of attitude determination and control of CubeSats with consideration of disturbances and system uncertainties. One of the challenges that accompany virtual telescope technology in aerospace engineering is the need for high-accuracy attitude alignment and a quick settling time to obtain images. Our results suggest a method to evaluate and analyze settling times for distributed space telescopes with the requirements of pointing accuracy and stability, specifically, for multiple CubeSat configurations. 


Last Modified: 02/12/2024
Modified by: Hyeongjun Park

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