NASA SBIR 2021-I Solicitation

Proposal Summary


   
Proposal Number:          21-1- Z8.02-3103
          
          
   
Subtopic Title:
      Communications and Navigation for Distributed Small Spacecraft Beyond Low Earth Orbit (LEO)
          
          
   
Proposal Title:
      Fault Tolerant Beam Steering for Cubesats
          
          

Small Business Concern

   
Firm:
          
Miles Space, Inc.
          
   
Address:
          
5007 West Nassau Street, Tampa, FL 33607
          
   
Phone:
          
(813) 249-5522                                                                                                                                                                                
          

Principal Investigator:

   
Name:
          
Wesley Faler
          
   
E-mail:
          
wes@miles-space.com
          
   
Address:
          
5007 W Nassau St, FL 33607 - 3814
          
   
Phone:
          
(734) 476-1437                                                                                                                                                                                
          

Business Official:

   
Name:
          
Wesley Faler
          
   
E-mail:
          
wes@miles-space.com
          
   
Address:
          
5007 W Nassau St, FL 33607 - 3814
          
   
Phone:
          
(734) 476-1437                                                                                                                                                                                
          

Summary Details:

   
Estimated Technology Readiness Level (TRL) :                                                                                                                                                          
Begin: 4
End: 5
          
          
     
Technical Abstract (Limit 2000 characters, approximately 200 words):

This proposal is an enabling communication technology for small spacecraft beyond LEO. We propose to adapt real-time coherent combining software for electronically steered arrays recently proven for ground-to-space communications to the computing constraints of small spacecraft. An electronically steered array antenna system must adjust the phase of multiple received signals so they coherently combine, with errors in the process rapidly degrading the output signal. The chief method of mitigating phase errors is to place the radio antenna elements into a robust, high precision mechanical structure. On a moving platform, another mitigation is also used, precise measurements of movement and/or cessation of all movement during antenna usage. The first is at direct odds with the need for small spacecraft to use lightweight, flexible, and deployable structures. The second is an extreme challenge for orbiting craft, especially those navigating in CisLunar or deep space where relative position knowledge is degraded compared to LEO satellite situations.

Miles Space’s coherent combining software continuously adapts to phase differences in radio data streams allowing them to be combined successfully, nearly eliminating grating lobes. Doing so allows flexible, deployable antennas to be used on rotating craft, even those that may have residual antenna vibration due to recent propulsion and attitude control usage. There are corresponding cost and risk reductions in craft mass and machining tolerances with improved tolerance to deployment mechanism issues and on-mission antenna damage.

Through a contract with ATLAS Space Operations, Miles Space demonstrated to the US Air Force its coherent combining software operating on a phased array ground terminal downlinking GEO and LEO satellite signals. The algorithm was used on digitized RF data before the data reached a commercial modem for decoding. As judged by the modem, real-time coherent combining eliminated grating lobes.

          
          
     
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

Dynamic coherent combining breaks constraints of phased array mounting. Arrays can be created from flexible structures, even operating while vibrating, tolerating off-plane rotation while still coherently combining signals, expanding mounting options on a mission.

Scientific missions benefit from placement flexibility, letting the science needs dominate.

CisLunar and deeper missions need high delta-v. Craft mass is lowered by using this algorithm to perform phase shifting on low mass, low volume deployable phased array antennas, raising delta-v.

          
          
     
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

Phased arrays let the commercial market obtain licensing in an ever more crowded orbit and this technology makes phased arrays far more economical and practical.

Military projects will benefit from this technology as well. The dynamic aspect of the software responds quickly to changing signal conditions, tolerating sudden changes due to damage, increasing resiliency and overall advantage.

          
          
     
Duration:     6
          
          

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