Master Clock Vibration-Isolation Technology Improvements for Aircraft Avionics
Navy SBIR 2011.2 - Topic N112-126
NAVAIR - Ms. Donna Moore - [email protected]
Opens: May 26, 2011 - Closes: June 29, 2011

N112-126 TITLE: Master Clock Vibration-Isolation Technology Improvements for Aircraft Avionics

TECHNOLOGY AREAS: Air Platform, Sensors, Electronics

ACQUISITION PROGRAM: PMA-272, Advanced Tactical Aircraft Protection Systems

OBJECTIVE: Develop a vibration-isolation schema that greatly improves by several magnitudes the performance of the 10-megahertz (MHz) master clock in aircraft avionics.

DESCRIPTION: Every digital receiver system that serves signal intelligence (SIGINT), electronics intelligence (ELINT), and communications intelligence (COMINT) has a crystal oscillator as a reference source (master clock). Also, every aviation platform has platform-induced vibration that adds random phase noise to these crystal oscillators, thereby increasing phase noise by as much as 45 decibels (dB) and degrading overall system performance. When receiving electronic signals of interest during collection events, aircraft experience vibration-induced phase noise that increases the noise floor creating the potential for failure to detect signals that are under the platform's noise floor. Further, the more vibration-induced phase noise there is, the smaller the platform stand-off range is, or the closer to the source the detection platform has to be.

In order to decrease the noise floor and increase the stand-off range of aviation platforms (UAVs included) that receive and gather electronic information, a novel approach to reducing the platform-induced vibration in the crystal oscillator is needed. Creating a novel vibration-isolation solution will reap overall system performance benefits throughout all avionics on the aircraft that use master clock reference signals, including radars, jammers, countermeasures, and so on.

PHASE I: Develop novel solutions to increase the vibration isolation of the crystal oscillator in legacy aircraft avionics. Provide both white paper theory and modeling and simulation as to the benefit of the proposed vibration-isolation schema. This modeling and simulation should show significant performance improvements of legacy avionics based on the crystal oscillator's improved vibration isolation.

PHASE II: Develop a prototype vibration-isolation solution and conduct platform-specified vibration analysis, demonstrating reduced vibration and increased receiver sensitivities. Vibration testing will include three aircraft-type vibration tables prescribed by the technical point of contact (TPOC) at the beginning of Phase II.

PHASE III: Transition the approach to legacy systems and other platforms that will benefit from the developed vibration-isolation schema.

PRIVATE SECTOR COMMERCIAL POTENTIAL/DUAL-USE APPLICATIONS: Every aircraft, military and commercial, has vibrations that affect the reference crystal oscillator (master clock), creating a degradation in the system's performance. Advances in vibration isolation for crystal oscillator applications will result in system improvements.

REFERENCES:
1. Driscoll, M. M. (2002, June). Low noise oscillator design and performance. Paper presented at the IEEE Frequency Control Symposium, New Orleans, LA. Retrieved from http://www.scribd.com/doc/14168533/Low-Noise-Oscillator-Design-and-Performance-MMDriscoll

2. Corsaro, R. D., Herdic, P. C., Houston, B. H., & Klunder, J. D. and assigned to the United States of America as represented by the Secretary of the Navy. (2009). U.S. Patent No. 7,586,236. Washington, DC: U.S. Patent and Trademark Office. Retrieved from http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PALL&p=1&u=%2Fnetahtml%2FPTO%2Fsrchnum.htm&r=1&f=G&l=50&s1=7586236.PN.&OS=PN/7586236&RS=PN/7586236

3. Vig, J. R. and assigned to the United States of America as represented by the Secretary of the Army. (1997). U.S. Patent No. 5,652,550. Washington, DC: U.S. Patent and Trademark Office. Retrieved from http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PALL&p=1&u=%2Fnetahtml%2FPTO%2Fsrchnum.htm&r=1&f=G&l=50&s1=5,652,550.PN.&OS=PN/5,652,550&RS=PN/5,652,550

4. Howe, D. A. (2006). Phase noise and vibration tolerance in microwave oscillators: Needs vs. state-of-the-art. Boulder, CO: National Institute of Standards and Technology. Retrieved from http://nistboulder.net/Presentations/HoweMTO%20DarpaPhotonicsConf06.pdf

KEYWORDS: crystal oscillator; vibration isolation; master clock; electronic warfare; decibel; vibration noise reduction

** TOPIC AUTHOR (TPOC) **
DoD Notice:  
Between April 26 and May 25, 2011, you may talk directly with the Topic Authors to ask technical questions about the topics. Their contact information is listed above. For reasons of competitive fairness, direct communication between proposers and topic authors is
not allowed starting May 26, 2011, when DoD begins accepting proposals for this solicitation.
However, proposers may still submit written questions about solicitation topics through the DoD's SBIR/STTR Interactive Topic Information System (SITIS), in which the questioner and respondent remain anonymous and all questions and answers are posted electronically for general viewing until the solicitation closes. All proposers are advised to monitor SITIS (11.2 Q&A) during the solicitation period for questions and answers, and other significant information, relevant to the SBIR 11.2 topic under which they are proposing.

If you have general questions about DoD SBIR program, please contact the DoD SBIR Help Desk at (866) 724-7457 or email weblink.