Small Spacecraft & Small Robot Lighting System for Navigation, Identification and Communications

Case ID:
UA24-189
Invention:

Spacecraft Optimized Lighting-communications Architecture for Robust Integrated Systems (SOLARIS) is a framework that utilizes advanced lighting and software to enhance communications, tracking, navigation, and security in small spacecraft and robotic systems such as rovers, CubeSats, and more. The framework outlines an entire system to integrate lighting into a spacecraft/space robot. Lighting display formats can be customized and can be connected by wire or wirelessly to host spacecraft or robots. SOLARIS also includes design software that balances design execution on spacecraft, rovers, space infrastructure based on task needs.

Whether designing lighting communication systems for small CubeSats or large interplanetary probes, SOLARIS scales to accommodate diverse spacecraft sizes and mission complexities. The modular architecture is customizable, allowing users to incorporate new lighting technologies, adapt to evolving mission requirements, and remain at the forefront of spacecraft illumination design. With SOLARIS, spacecraft designers can confidently create illumination systems that optimize energy efficiency, enhance scientific observations, and support the success of missions, from LEO to Cislunar space to deep space.

Background: 
As space traffic increases exponentially, effective space traffic management becomes imperative to prevent collisions and ensure uninhibited movement. Moreover, the preservation of satellite assets in orbit, pivotal for sustaining essential services on Earth, enhances the urgency of optimizing spacecraft operations. 

Applications: 

  • Light-based communications system for use with:
    • Small spacecraft
    • CubeSats
    • Rovers
    • Other space-based robotic systems


Advantages: 

  • Performs visual communication
  • Customizable lighting display formats
  • Enhances communications, tracking, navigation, and security
  • Scalable for different spacecraft sizes
  • Can work with wired or wireless connection
Patent Information:
Contact For More Information:
Scott Zentack
Licensing Manager, College of Engr
The University of Arizona
szentack@arizona.edu
Lead Inventor(s):
Jekan Thangavelautham
Athip Thirupathi Raj
Jaret Rickel
Roshan Adhikari
Keywords: