TY - GEN
T1 - Use of laser beams to configure and command spacecraft swarms
AU - Kalita, Himangshu
AU - Vance, Leonard Dean
AU - Reddy, Vishnu
AU - Thangavelautham, Jekan
N1 - Publisher Copyright:
© 2019, Univelt Inc. All rights reserved.
PY - 2019
Y1 - 2019
N2 - The availability of high-performance Commercial Off-The-Shelf (COTS) electronics that can withstand Low Earth Orbit conditions has opened avenue for wide deployment of CubeSats and small-satellites. Utilizing many scores, if not hundreds of these satellites can provide services to end-users on the ground such as position, navigation and tracking (PNT), persistent earth imaging, secure communications and off-grid data storage. Not all these satellites operate as intended in space and some may face premature failure and others may become immobile. This requires effective traffic management. In our approach, a secure laser beam will be used to directly communicate gestures and control one or more spacecraft, including a swarm. Each satellite will have a customized “smart skin” containing solar panels, power and control circuitry and an embedded secondary propulsion unit. A secondary propulsion unit may include electrospray propulsion, solar radiation pressure-based system, photonic laser thrusters and Lorentz force thrusters. Solar panels typically occupy the largest surface area on an earth orbiting satellite. Furthermore, our previous work has shown that commercial space-grade solar panels can be used to detect and distinguish blue and purple laser beams even when exposed to sunlight. A secure laser beam from another spacecraft or from the ground would interact with solar panels of the spacecraft. In a swarm, the secure laser beam would be used to first designate a temporary leader of the swarm, followed by configuration of the spacecraft swarm formation. In this paper we present a low-cost on-orbit mission concept to demonstrate the technology using a pair of 2U CubeSats and a dozen SunCube 1F FemtoSats. Using this low-cost mission, we hope to validate the technology in space.
AB - The availability of high-performance Commercial Off-The-Shelf (COTS) electronics that can withstand Low Earth Orbit conditions has opened avenue for wide deployment of CubeSats and small-satellites. Utilizing many scores, if not hundreds of these satellites can provide services to end-users on the ground such as position, navigation and tracking (PNT), persistent earth imaging, secure communications and off-grid data storage. Not all these satellites operate as intended in space and some may face premature failure and others may become immobile. This requires effective traffic management. In our approach, a secure laser beam will be used to directly communicate gestures and control one or more spacecraft, including a swarm. Each satellite will have a customized “smart skin” containing solar panels, power and control circuitry and an embedded secondary propulsion unit. A secondary propulsion unit may include electrospray propulsion, solar radiation pressure-based system, photonic laser thrusters and Lorentz force thrusters. Solar panels typically occupy the largest surface area on an earth orbiting satellite. Furthermore, our previous work has shown that commercial space-grade solar panels can be used to detect and distinguish blue and purple laser beams even when exposed to sunlight. A secure laser beam from another spacecraft or from the ground would interact with solar panels of the spacecraft. In a swarm, the secure laser beam would be used to first designate a temporary leader of the swarm, followed by configuration of the spacecraft swarm formation. In this paper we present a low-cost on-orbit mission concept to demonstrate the technology using a pair of 2U CubeSats and a dozen SunCube 1F FemtoSats. Using this low-cost mission, we hope to validate the technology in space.
UR - http://www.scopus.com/inward/record.url?scp=85079487584&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85079487584&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85079487584
SN - 9780877036616
T3 - Advances in the Astronautical Sciences
SP - 979
EP - 990
BT - Guidance, Navigation, and Control, 2019
A2 - Hallowell, Heidi E.
PB - Univelt Inc.
T2 - 42nd AAS Rocky Mountain Section Guidance and Control Conference, 2019
Y2 - 31 January 2019 through 6 February 2019
ER -