Precise Robust Inertial Guidance for Munitions: Advanced Inertial Micro Sensors (PRIGM:AIMS)
Amendment 01:
The purpose of this amendment is to revise/clarify the travel related funding restrictions, and to correct a Coriolis Vibratory Gyroscopes (CVG) Class typo.
All changes made to the BAA are highlighted in yellow.
See the attached DARPA-BAA-15-38 document through Amendment 0 1. The DARPA Microsystems Technology Office is soliciting research proposals in the development of novel technologies for high-performance miniature inertial sensors.
The PRIGM:AIMS program will address the challenge of precise navigation of guided munitions in the absence of external navigation aids, such as GPS.
This BAA is particularly interested in inertial sensors that enable precision navigation of gun-launched spin-stabilized munitions, as well as the navigation of highly dynamic, long-range munitions.
PRIGM:AIMS will investigate and demonstrate new sensing modalities for low-Cost, Size, Weight and Power (CSWaP) inertial sensors including, but not limited to:
rate-integrating gyroscopes, integrated photonic waveguide optical gyroscopes, and optically-interrogated MEMS gyroscopes and accelerometers.
See the full DARPA-BAA-15-38 document attached.
The purpose of this amendment is to revise/clarify the travel related funding restrictions, and to correct a Coriolis Vibratory Gyroscopes (CVG) Class typo.
All changes made to the BAA are highlighted in yellow.
See the attached DARPA-BAA-15-38 document through Amendment 0 1. The DARPA Microsystems Technology Office is soliciting research proposals in the development of novel technologies for high-performance miniature inertial sensors.
The PRIGM:AIMS program will address the challenge of precise navigation of guided munitions in the absence of external navigation aids, such as GPS.
This BAA is particularly interested in inertial sensors that enable precision navigation of gun-launched spin-stabilized munitions, as well as the navigation of highly dynamic, long-range munitions.
PRIGM:AIMS will investigate and demonstrate new sensing modalities for low-Cost, Size, Weight and Power (CSWaP) inertial sensors including, but not limited to:
rate-integrating gyroscopes, integrated photonic waveguide optical gyroscopes, and optically-interrogated MEMS gyroscopes and accelerometers.
See the full DARPA-BAA-15-38 document attached.
Agency: Department of Defense
Office: Defense Advanced Research Projects Agency
Estimated Funding: Not Available
Office: Defense Advanced Research Projects Agency
Estimated Funding: Not Available
Obtain Full Opportunity Text:
MTO Solicitations Page
Additional Information of Eligibility:
Not Available
Full Opportunity Web Address:
http://www.darpa.mil/Opportunities/Solicitations/DARPA_Solicitations.aspx#MTO
Contact:
Robert Lutwak, Program Manager
Agency Email Description:
BAA Coordinator
Agency Email:
DARPA-BAA-15-38@darpa.mil
Date Posted:
2015-05-29
Application Due Date:
2015-09-10
Archive Date:
2016-03-31
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