DARPA (DSO): Precision Inertial Navigation and Positioning On an Integrated Tesseract (PINPOINT)

The objective of PINPOINT is to develop new physics and nonlinear control methodologies to deliver proof-of-concept six-degree-of-freedom (6-DOF) IMUs meeting the requirements of DoW-relevant missions. For Phase I, performers will first demonstrate the mathematical rigor and simulation results of their advanced non-linear systems and dynamic state estimators and perform laboratory testing of foundational inertial-sensor and IMU performance וsing bench-top evaluations.

Funding: no fixed limit
Duration: 2 years

Research Authority due date: 19.8.26
Abstract (required) due date: 27.8.26
Full proposal due date: 25.9.26